EuroPak-15a/15aT
Receiver
USER MANUAL
OM-20000100
Rev 5
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Table of Contents
1.3.2 Commercial Service............................................................................................................. 18
1.3.3 Safety-of-Life Service........................................................................................................... 19
1.3.4 Public Regulated Service..................................................................................................... 19
1.7.1 Radio Frequency Section..................................................................................................... 21
1.8 Antenna or Signal Generator......................................................................................................... 22
2.2.2 Connecting the Antenna or Signal Generator to the Receiver............................................. 25
2.2.3 Applying Power to the Receiver........................................................................................... 26
2.3.1 Strobes................................................................................................................................. 26
2.3.3 External Oscillator................................................................................................................ 27
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Table of Contents
4.1 Entering Commands...................................................................................................................... 31
4.1.3 Response Formats............................................................................................................... 32
4.3.1 ASCII.................................................................................................................................... 35
4.4.2 Commonly-Used Fields........................................................................................................ 39
5.3.1 AGCMODE Control Automatic Gain Control ..................................................................... 45
5.3.2 ASSIGN Assign Individual Satellite Channels ................................................................... 47
5.3.4 CLOCKADJUST................................................................................................................... 50
5.3.5 COM Serial Port Configuration Control.............................................................................. 51
5.3.6 ECUTOFF Set Satellite Elevation Cut-off.......................................................................... 53
5.3.7 EXTERNALCLOCK.............................................................................................................. 54
5.3.8 FIX Constrain to Fixed Position ......................................................................................... 56
5.3.9 FRESET Clear Data in NVM.............................................................................................. 58
5.3.10 LOG Request Logs from Receiver................................................................................... 59
5.3.11 POSITIONTYPE Set the Position Solution...................................................................... 61
5.3.12 PULSEBLANKING Enable/Disable Pulse Blanking......................................................... 62
5.3.13 RESET Hardware Reset.................................................................................................. 63
5.3.14 SDLLBW Configure DLL Filter Bandwidth....................................................................... 64
5.3.15 SPLLBW Configure Phase-Lock-Loop Bandwidth........................................................... 65
5.3.16 STHRESHOLD Control Signal Thresholds...................................................................... 66
5.3.17 UNASSIGN Unassign a Previously Assigned Channel ................................................... 67
5.3.18 UNLOG Remove Log from Logging Control.................................................................... 68
5.3.19 UNLOGALL Remove All Logs from Logging Control....................................................... 69
6.1 Functional Listing of Logs.............................................................................................................. 70
6.3.1 AGCSTATS Automatic Gain Control Status...................................................................... 72
6.3.2 ALMANAC Decoded Almanac........................................................................................... 75
6.3.3 CLOCKMODEL Current Clock Model Status..................................................................... 77
6.3.4 PSRPOS Pseudorange Position........................................................................................ 80
6.3.5 RANGE Satellite Range Information.................................................................................. 82
6.3.6 RAWEPHEM Raw Ephemeris ........................................................................................... 86
6.3.7 RAWFRAME Raw Subframes ........................................................................................... 87
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Table of Contents
6.3.8 RXCOMMANDS Receiver Configuration........................................................................... 88
6.3.9 RXSECSTATUS Receiver Section Status......................................................................... 91
6.3.10 SATVIS Satellite Visibility................................................................................................ 94
6.3.11 SYSTEMLEVELS System Hardware Levels ................................................................... 96
6.3.12 TIME Time Data .............................................................................................................. 97
6.3.13 TRACKSTAT Tracking Status ......................................................................................... 98
6.3.14 VERSION Version Information ...................................................................................... 100
7.1 Contacting the NovAtel Aviation Department .............................................................................. 102
7.2 Downloading the Files ................................................................................................................. 103
7.3 Decompressing the Files ............................................................................................................. 103
7.4 Running the Utility........................................................................................................................ 104
8.4.3 Status Code Arrays............................................................................................................ 109
8.4.5 Auxiliary Status Codes....................................................................................................... 109
Appendices
A Technical Specifications
110
125
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Figures
Main Screen of WinLoad............................................................................................................. 104
COM Port Setup.......................................................................................................................... 105
Location of Receiver Error Word................................................................................................. 108
EuroPak-15a Straight Through Serial Cable............................................................................... 117
EuroPak-15a I/O Strobe Port Cable............................................................................................ 118
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Tables
Available Strobe Signals on the EuroPak-15a ............................................................................. 27
EuroPak-15a Status Indicators .................................................................................................... 27
Byte Arrangements ...................................................................................................................... 39
GPS Time Status ........................................................................................................................ 40
Command Summary .................................................................................................................... 44
AGC Mode Values ....................................................................................................................... 45
Antispoofing Flag Values ............................................................................................................. 46
Channel State Values .................................................................................................................. 48
Handshaking Values .................................................................................................................... 52
Clock Type ................................................................................................................................... 55
Fix Type Values ........................................................................................................................... 56
Logs By Function ......................................................................................................................... 70
Clock Model Status Values .......................................................................................................... 79
Position Type Values ................................................................................................................... 81
Correlator Spacing Bit Values ...................................................................................................... 85
Satellite Visibility Values .............................................................................................................. 95
Reject Code Values ..................................................................................................................... 99
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Tables
Static-Accumulating Materials .................................................................................................... 124
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Notices
Notices
The following notices apply to the EuroPak-15a.
FCC NOTICE
This equipment has been tested and found to comply with the radiated and conducted emission limits for a
Class B digital device, for both CISPR 22 and Part 15 of the FCC rules. These limits are designed to provide
reasonable protection against harmful interference in a residential installation. This equipment generates, uses,
and can radiate radio frequency energy and, if not installed and used in accordance with the instructions, may
cause harmful interference to radio communications. However, there is no guarantee that interference will not
occur in a particular installation. If this equipment does cause harmful interference to radio or television
reception, which can be determined turning the equipment off and on, the user is encouraged to try to correct
the interference by one or more of the following measures:
• Re-orient or relocate the receiving antenna
• Increase the separation between the equipment and the receiver
• Connect the equipment to an outlet on a circuit different from that to which the receiver is
connected
• Consult the dealer or an experienced radio/TV technician for help
IMPORTANT:
In order to maintain compliance with the limits of a Class B digital device, it is required to
use properly shielded interface cables (such as Belden #9539 or equivalent) when using the
serial data ports, and double-shielded cables (such as Belden #9945 or equivalent) when
using the I/O strobe port.
WARNING: Changes or modifications to this equipment not expressly approved by NovAtel Inc. could
result in violation of Part 15 of the FCC rules.
CE NOTICE
The enclosure carries the CE mark.
WARNING: This is a Class B product. In a domestic environment this product may cause radio
interference in which case the user may be required to take adequate measures.
"Hereby, NovAtel Inc. declares that this EuroPak-15a is in compliance with the essential requirements and
other relevant provisions of Directive 1999/5/EC."
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Notices
Electromagnetic Compatibility (EMC)
The EuroPak-15a has passed the following EMC regulatory tests:
Emissions Testing of the EUROPAK-15a
•
•
EN 55022 1998 (CISPR 22 (2006)) - Information technology equipment - Radio disturbance
characteristics - Limits and methods of measurement
FCC, Part 15 Subpart B (2004)
Immunity Testing of the EUROPAK–15a
EN 61000-6-1: 2001 – Immunity Requirements for Residential, Commercial and Light
Industrial Environments
•
Safety of Information Technology Equipment
IEC/EN 60950
•
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Software License
Software License
BY INSTALLING, COPYING, OR OTHERWISE USING THE SOFTWARE PRODUCT, YOU AGREE
TO BE BOUND BY THE TERMS OF THIS AGREEMENT. IF YOU DO NOT AGREE TO THE TERMS
OF THIS AGREEMENT, DO NOT INSTALL, COPY OR USE THE SOFTWARE PRODUCT.
1. License: NovAtel Inc. ("NovAtel") grants you a non-exclusive, non-transferable license (not a sale) to use
one copy of the enclosed NovAtel software on a single computer, and only with the product it was supplied
with. You agree not to use the software for any purpose other than the due exercise of the rights and
licences hereby agreed to be granted to you.
2. Copyright: NovAtel owns, or has the right to sublicense, all copyright, trade secret, patent and other
proprietary rights in the software and the software is protected by national copyright laws, international
treaty provisions and all other applicable national laws. You must treat the software like any other
copyrighted material except that you may either (a) make one copy of the software solely for backup or
archival purposes, the media of said copy shall bear labels showing all trademark and copyright notices
that appear on the original copy, or (b) transfer the software to a single hard disk provided you keep the
original solely for backup or archival purposes. You may not copy the product manual or written materials
accompanying the software. No right is conveyed by this Agreement for the use, directly, indirectly, by
implication or otherwise by Licensee of the name of NovAtel, or of any trade names or nomenclature used
by NovAtel, or any other words or combinations of words proprietary to NovAtel, in connection with this
Agreement, without the prior written consent of NovAtel.
3. Patent Infringement: NovAtel shall not be liable to indemnify the Licensee against any loss sustained by it
as the result of any claim made or action brought by any third party for infringement of any letters patent,
registered design or like instrument of privilege by reason of the use or application of the software by the
Licensee or any other information supplied or to be supplied to the Licensee pursuant to the terms of this
Agreement. NovAtel shall not be bound to take legal proceedings against any third party in respect of any
infringement of letters patent, registered design or like instrument of privilege which may now or at any
future time be owned by it. However, should NovAtel elect to take such legal proceedings, at NovAtel's
request, Licensee shall co-operate reasonably with NovAtel in all legal actions concerning this license of
the software under this Agreement taken against any third party by NovAtel to protect its rights in the
software. NovAtel shall bear all reasonable costs and expenses incurred by Licensee in the course of co-
operating with NovAtel in such legal action.
4. Restrictions: You may not: (1) copy (other than as provided for in paragraph 2), distribute, transfer, rent,
lease, lend, sell or sublicense all or any portion of the software; (2) modify or prepare derivative works of
the software; (3) use the software in connection with computer-based services business or publicly display
visual output of the software; (4) transmit the software over a network, by telephone or electronically using
any means; or (5) reverse engineer, decompile or disassemble the software. You agree to keep confidential
and use your best efforts to prevent and protect the contents of the software from unauthorized disclosure
or use.
5. Term and Termination: This Agreement and the rights and licences hereby granted shall continue in force
in perpetuity unless terminated by NovAtel or Licensee in accordance herewith. In the event that the
Licensee shall at any time during the term of this Agreement: i) be in breach of its obligations hereunder
where such breach is irremediable or if capable of remedy is not remedied within 30 days of notice from
NovAtel requiring its remedy; or ii) be or become bankrupt or insolvent or make any composition with its
creditors or have a receiver or manager appointed of the whole or any part of its undertaking or assets or
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Software License
(otherwise as a solvent company for the purpose of and followed by an amalgamation or reconstruction
hereunder its successor shall be bound by its obligations hereunder) commence to be wound up; or iii) be
acquired or otherwise come under the direct or indirect control of a person or persons other than those
controlling it, then and in any event NovAtel may forthwith by notice in writing terminate this Agreement
together with the rights and licences hereby granted by NovAtel. Licensee may terminate this Agreement
by providing 30 days prior written notice to NovAtel. Upon termination, for any reasons, the Licensee shall
promptly, on NovAtel's request, return to NovAtel or at the election of NovAtel destroy all copies of any
documents and extracts comprising or containing the software. The Licensee shall also erase any copies of
the software residing on Licensee's computer equipment. Termination shall be without prejudice to the
accrued rights of either party, including payments due to NovAtel. This provision shall survive termination
of this Agreement howsoever arising.
6. Warranty: For 90 days from the date of shipment, NovAtel warrants that the media (for example, compact
disk) on which the software is contained will be free from defects in materials and workmanship. This
warranty does not cover damage caused by improper use or neglect. NovAtel does not warrant the contents
of the software or that it will be error free. The software is furnished "AS IS" and without warranty as to the
performance or results you may obtain by using the software. The entire risk as to the results and
performance of the software is assumed by you.
7. Indemnification: NovAtel shall be under no obligation or liability of any kind (in contract, tort or otherwise
and whether directly or indirectly or by way of indemnity contribution or otherwise howsoever) to the
Licensee and the Licensee will indemnify and hold NovAtel harmless against all or any loss, damage,
actions, costs, claims, demands and other liabilities or any kind whatsoever (direct, consequential, special
or otherwise) arising directly or indirectly out of or by reason of the use by the Licensee of the software
whether the same shall arise in consequence of any such infringement, deficiency, inaccuracy, error or
other defect therein and whether or not involving negligence on the part of any person.
8. For software UPDATES and UPGRADES, and regular customer support, contact the NovAtel GPS Hotline
at 1-800-NOVATEL (U.S. or Canada only), or 403-295-4900, or fax 403-295-4901, e-mail to
[email protected], visit our website http://www.novatel.com or write to:
NOVATEL INC.
CUSTOMER SERVICE DEPT.
1120 - 68 AVENUE NE,
CALGARY, ALBERTA, CANADA T2E 8S5
9. Disclaimer of Warranty and Limitation of Liability:
a. THE WARRANTIES IN THIS AGREEMENT REPLACE ALL OTHER WARRANTIES, EXPRESS
OR IMPLIED, INCLUDING ANY WARRANTIES OF MERCHANTABILITY OR FITNESS FOR A
PARTICULAR PURPOSE. NovAtel DISCLAIMS AND EXCLUDES ALL OTHER WARRANTIES.
IN NO EVENT WILL NovAtel's LIABILITY OF ANY KIND INCLUDE ANY SPECIAL,
INCIDENTAL OR CONSEQUENTIAL DAMAGES, INCLUDING LOST PROFITS, EVEN IF
NovAtel HAS KNOWLEDGE OF THE POTENTIAL LOSS OR DAMAGE.
b. NovAtel will not be liable for any loss or damage caused by delay in furnishing the software or any other
performance under this Agreement.
c. NovAtel's entire liability and your exclusive remedies for our liability of any kind (including liability
for negligence) for the software covered by this Agreement and all other performance or non-perfor-
mance by NovAtel under or related to this Agreement are to the remedies specified by this Agreement.
This Agreement is governed by the laws of the Province of Alberta, Canada. Each of the parties
hereto irrevocably attorns to the jurisdiction of the courts of the Province of Alberta.
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Warranty Policy
Warranty Policy
NovAtel Inc. warrants that its Global Positioning System (GPS) products are free from defects in materials and
workmanship, subject to the conditions set forth below, for the following periods of time:
EuroPak-15a Receivers
NovAtel Antennas
Cables and Accessories
Software Support
One (1) Year from date of sale
One (1) Year from date of sale
Ninety (90) Days from date of sale
One (1) Year from date of sale
Date of sale shall mean the date of the invoice to the original customer for the product. NovAtel’s responsibility
respecting this warranty is solely to product replacement or product repair at an authorized NovAtel location.
Determination of replacement or repair will be made by NovAtel personnel or by technical personnel expressly
authorized by NovAtel for this purpose.
THE FOREGOING WARRANTIES DO NOT EXTEND TO (I) NONCONFORMITIES, DEFECTS OR
ERRORS IN THE PRODUCTS DUE TO ACCIDENT, ABUSE, MISUSE OR NEGLIGENT USE OF
THE PRODUCTS OR USE IN OTHER THAN A NORMAL AND CUSTOMARY MANNER, ENVI-
RONMENTAL CONDITIONS NOT CONFORMING TO NOVATEL’S SPECIFICATIONS, OR FAIL-
URE TO FOLLOW PRESCRIBED INSTALLATION, OPERATING AND MAINTENANCE
PROCEDURES, (II) DEFECTS, ERRORS OR NONCONFORMITIES IN THE PRODUCTS DUE TO
MODIFICATIONS, ALTERATIONS, ADDITIONS OR CHANGES NOT MADE IN ACCORDANCE
WITH NOVATEL’S SPECIFICATIONS OR AUTHORIZED BY NOVATEL, (III) NORMAL WEAR
AND TEAR, (IV) DAMAGE CAUSED BY FORCE OF NATURE OR ACT OF ANY THIRD PERSON,
(V) SHIPPING DAMAGE; OR (VI) SERVICE OR REPAIR OF PRODUCT BY THE DEALER WITH-
OUT PRIOR WRITTEN CONSENT FROM NOVATEL. IN ADDITION, THE FOREGOING WAR-
RANTIES SHALL NOT APPLY TO PRODUCTS DESIGNATED BY NOVATEL AS BETA SITE TEST
SAMPLES, EXPERIMENTAL, DEVELOPMENTAL, PREPRODUCTION, SAMPLE, INCOMPLETE
OR OUT OF SPECIFICATION PRODUCTS OR TO RETURNED PRODUCTS IF THE ORIGINAL
IDENTIFICATION MARKS HAVE BEEN REMOVED OR ALTERED. THE WARRANTIES AND
REMEDIES ARE EXCLUSIVE AND ALL OTHER WARRANTIES, EXPRESS OR IMPLIED, WRIT-
TEN OR ORAL, INCLUDING THE IMPLIED WARRANTIES OF MERCHANTABILITY OR FIT-
NESS FOR ANY PARTICULAR PURPOSE ARE EXCLUDED. NOVATEL SHALL NOT BE LIABLE
FOR ANY LOSS, DAMAGE, EXPENSE, OR INJURY ARISING DIRECTLY OR INDIRECTLY OUT
OF THE PURCHASE, INSTALLATION, OPERATION, USE OR LICENSING OR PRODUCTS OR
SERVICES. IN NO EVENT SHALL NOVATEL BE LIABLE FOR SPECIAL, INDIRECT, INCIDEN-
TAL OR CONSEQUENTIAL DAMAGES OF ANY KIND OR NATURE DUE TO ANY CAUSE.
There are no user serviceable parts in the GPS receiver and no maintenance is required. When the status code indicates
that a unit is faulty, replace with another unit and return the faulty unit to NovAtel Inc.
Before shipping any material to NovAtel or Dealer, please obtain a Return Material Authorization (RMA)
number from the point of purchase. You may also visit our website at http://www.novatel.com and select
Support | Repair Request from the side menu.
Once you have obtained an RMA number, you will be advised of proper shipping procedures to return any defective
product. When returning any product to NovAtel, please return the defective product in the original packaging to avoid
ESD and shipping damage.
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Customer Service
Customer Service
Contact Information
If you have any questions or concerns regarding your EuroPak-15a receiver, please contact the NovAtel
Aviation Group using any one of the following methods:
NovAtel GPS Hotline:
1-800-NOVATEL (U.S. and Canada)
403-295-4900 (International)
Fax:
403-295-4999
E-mail:
Website:
Write:
NovAtel Inc. Aviation Group
1120 - 68 Avenue NE
Calgary, Alberta, Canada
T2E 8S5
Firmware Updates
Firmware updates are firmware revisions to an existing model, which improve basic functionality of the GPS
receiver.
The process for obtaining firmware updates is discussed in Chapter 7, Firmware Updates starting on Page 102.
If you need further information, please contact NovAtel using one of the methods given above.
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Foreword
Foreword
Scope
This manual contains sufficient information on the installation and operation of the EuroPak-15a or EuroPak-
15aT receiver to allow you to effectively integrate and fully operate it. After the addition of accessories, user-
supplied data communications equipment and a power supply, the receiver is ready to go.
These receivers utilizes a comprehensive user-interface command structure, which requires communications
through its communications (COM) ports. This manual also lists and describes the various receiver commands
and logs.
For an overview of GPS, a glossary of terms, units of conversion and acronyms, refer to the GPS+ Reference
Manual available on our website at http://www.novatel.com/Downloads/docupdates.html.
It is beyond the scope of this manual to provide details on service or repair. Please contact your local NovAtel
Prerequisites
The installation chapters of this document provide information concerning the installation requirements and
considerations for the EuroPak-15a and EuroPak-15aT receivers.
Conventions
The term EuroPak-15aT will not be used in this manual unless a specific detail refers to it alone. The term
receiver and the term EuroPak-15a will infer that the text is applicable to a EuroPak-15a or EuroPak-15aT
unless otherwise stated.
The conventions used throughout this document are:
H
The letter H in the Binary Bytes or Binary Offset columns represents the header length for that
0x
A number following 0xis a hexadecimal number.
field
Text surrounded by a box indicates a variable parameter to be entered as part of the command string.
[ ]
< >
Parameters surrounded by [ and ] are optional in a command or are required for only some instances
of the command depending on the values of other parameters.
Text displayed between < and > indicates the entry of a keystroke in the case of the command or an
automatic entry in the case of carriage return <CR> and line feed <LF> in data output.
In tables where no values are given, such fields should be assumed to be reserved for future use.
Compliance with GPS Week Rollover
The GPS week rollover issue refers to the way GPS receivers store information regarding the current GPS
week. According to the official GPS system specifications document (ICD-GPS-200, paragraph 20.3.3.3.1.1),
"… 10 bits shall represent the number of the current GPS week…". This means the GPS week is represented by
an integer number between 0 and 1023. As GPS time started on Sunday January 6, 1980 at 0:00 hours, week
1023 ended on Saturday August 21, 1999 at 23:59:59.
As per the GPS system specifications document, NovAtel firmware resets the receiver's GPS week number
back to zero. Users should be aware of this issue and keep in mind that there may be a compatibility issue when
purchasing and using different makes of GPS receivers.
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Chapter 1
Introduction
This chapter provides information on the features and functionality of the EuroPak-15a and how it operates in
the context of an SBAS system.
1.1 Overview of the EuroPak-15a
The EuroPak-15a is a high-performance GPS, Galileo and GEO receiver capable of receiving and tracking
sixteen GPS L1, GPS L5, Galileo L1 and Galileo E5a signals. Alternatively, four of the sixteen signals can be
SBAS GEO L1 and SBAS GEO L5 signals. The EuroPak-15a also decodes the navigation signals.
There is flexibility in areas such as configuration and specification of output data and control signals. Multiple
software models are available, allowing you to better fit the receiver to the application while maintaining the
option for a compatible upgrade path.
The EuroPak-15a enclosure offers a complete solution, a protective enclosure that provides an interface to the
receiver card’s power, data, and status signals.
1.2 SBAS Overview
A Satellite-Based Augmentation System (SBAS) is a safety-critical system designed to augment the
Department of Defense Global Positioning System (GPS) Standard Positioning Service (SPS). SBAS enhances
GPS service by providing:
•
•
•
a ranging function to the SBAS satellites, which improves signal availability and reliability
GPS signal corrections, which improve accuracy
integrity monitoring, which improves safety
The primary mission of the SBAS system is to provide a means for air navigation for all phases of flight in the
National Airspace System (NAS) from departure, through en route, and approach. The principal functions of
SBAS include:
•
•
•
•
•
•
•
determining ionospheric corrections
determining satellite orbits
determining satellite clock corrections
determining satellite integrity
independent data verification
SBAS message broadcast and ranging
system operations & maintenance
As shown in Figure 1 on Page 17, the SBAS system consists of a series of Reference Stations and Master
Stations, a Ground Uplink Subsystem, and Geostationary Satellites (GEOs). The Reference Stations, which are
strategically located to provide adequate coverage, pick up GPS satellite data and route it to the Master
Stations. The Master Stations then process the data to determine the signal integrity, signal corrections, and
residual errors for each monitored satellite. This information is sent to the Ground Uplink Subsystem for
transmission to the GEOs, which then re-transmits the data on the GPS L1 and L5 (not yet available)
frequency. In the future, the system will support L5 signal frequency broadcasts.
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Introduction
Chapter 1
Figure 1: The SBAS Concept
Reference
Description
1
Geo satellite
2
GPS satellite constellation
3
L1 and L5
4
C1 and C5
5
GPS user
6
7
Integrity data, differential corrections and ranging control
Reference station
8
Master station
9
10
Integrity data, differential corrections, time control and status
Ground uplink subsystem
1.3 Galileo Overview
Galileo will be Europe's own global navigation satellite system, providing a highly accurate, guaranteed global
positioning service under civilian control. It will be inter-operable with GPS and GLONASS, the two other
global satellite navigation systems.
A user will be able to take a position with the same receiver from any of the satellites in any combination. By
offering dual frequencies as standard, however, Galileo will deliver real-time positioning accuracy down to the
metre range, which is unprecedented for a publicly available system.
It will guarantee availability of the service under all but the most extreme circumstances and will inform users
within seconds of a failure of any satellite. This will make it suitable for applications where safety is crucial,
such as running trains, guiding cars and landing aircraft.
The first experimental satellite, part of the so-called Galileo System Test Bed (GSTB) was launched in
December 2005. The objective of this experimental satellite is to characterize the critical technologies, which
are already in development under European Space Agency (ESA) contracts. Thereafter up to four operational
satellites will be launched in the 2007-2008 time frame to validate the basic Galileo space and related ground
segment. Once this In-Orbit Validation (IOV) phase has been completed, the remaining satellites will be
installed to reach the Full Operational Capability (FOC) in 2010.
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Chapter 1
Introduction
The fully deployed Galileo system consists of 30 satellites (27 operational + 3 active spares), positioned in
three circular Medium Earth Orbit (MEO) planes in 23616 km altitude above the Earth, and at an inclination of
the orbital planes of 56 degrees with reference to the equatorial plane. Once this is achieved, the Galileo
navigation signals will provide a good coverage even at latitudes up to 75 degrees north, which corresponds to
the North Cape, and beyond. The large number of satellites together with the optimization of the constellation,
and the availability of the three active spare satellites, will ensure that the loss of one satellite has no discernible
effect on the user.
Two Galileo Control Centres (GCC) will be implemented on European ground to provide for the control of the
satellites and to perform the navigation mission management. The data provided by a global network of twenty
Galileo Sensor Stations (GSS) will be sent to the Galileo Control Centres through a redundant communications
network. The GCC's will use the data of the Sensor Stations to compute the integrity information and to
synchronize the time signal of all satellites and of the ground station clocks. The exchange of the data between
the Control Centres and the satellites will be performed through so-called up-link stations. Five S-band up-link
stations and 10 C-band up-link stations will be installed around the globe for this purpose.
As a further feature, Galileo will provide a global Search and Rescue (SAR) function, based on the operational
search and rescue satellite aided tracking Cospas-Sarsat system. To do so, each satellite will be equipped with a
transponder, which is able to transfer the distress signals from the user transmitters to the Rescue Co-ordination
Centre (RCC), which will then initiate the rescue operation. At the same time, the system will provide a signal
to the user, informing them that their situation has been detected and that help is under way. This latter feature
is new and is considered a major upgrade compared to the existing system, which does not provide a feedback
to the user.
Five categories of services have been defined:
1. A free Open Service (OS)
2. A highly reliable Commercial Service (CS)
3. A Safety-of-Life Service (SOL)
4. A government encrypted Public Regulated Service (PRS)
5. A Search and Rescue Service (SAR)
1.3.1
Open Service
This single-frequency service will involve the provision of a positioning, navigation and precise timing service.
It will be available for use by any person in possession of a Galileo receiver. No authorization will be required
to access this service. Galileo is expected to be similar to GPS in this respect.
The principal applications will be general navigation and positioning, network timing, traffic information
systems, systems including information on alternative routes in the event of congestion, and wireless location,
for example, with mobile telephones.
Studies clearly show that the availability of these services will be significantly enhanced by the existence of a
greater number of satellites, as is the case when both GPS and Galileo are in operation. This is particularly
important for land-based services, such as private car navigation, where service is mostly required in downtown
cores and where satellite shadowing is minimized by the combination of the systems.
The Open Service will be transmitted in the E5a frequency band at 1176.45 MHz.
1.3.2
Commercial Service
Service providers using the multi-frequency commercial services will have the opportunity to give added value
to their range of products for which they can charge the end customer and will, in turn, pay a fee to the Galileo
operator. The signal will contain data relating to the additional commercial services being offered. In return for
the fee, the Galileo operator will be able to offer certain service guarantees. This aspect of service guarantee
and the commensurate liabilities is one area where Galileo is significantly differentiated from GPS. A key
component in achieving this is an independent system within Galileo for monitoring the satisfactory working of
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Introduction
the system and informing the end user of this by an integrity signal incorporated in the data stream.
Chapter 1
The main applications for this service concern professional users who are ready to pay for a service guaranteed
by the Galileo operator, notably in the areas of technical surveys, in activities involving customs and excise
operations, network synchronization, sea fleet management, vehicle fleet management, and road tolls.
Controlled access to this service for end-users and the providers of value-added services will be based on
protected access keys in the receivers. This will also enable revenue to be collected from users.
The commercial service will be transmitted in the E6 frequency band at 1278.75 MHz.
1.3.3
Safety-of-Life Service
The safety-of-life service will be offered to users who are highly dependant on precision, signal quality and
signal transmission reliability. It will offer a high level of integrity, and consequently, provide the user with a
very rapid warning of any possible malfunctions. It will need to be certified in accordance with the regulations
applicable to the various modes of transport (the International Civil Aviation Organization (ICAO) regulations
in the case of air transport; the International Maritime Organization (IMO) regulations in the case of sea
transport). This service will require specialized receivers providing access to this enhanced-quality signal.
The safety-of-life service will be transmitted in two frequency bands – L1 at 1575.42 MHz, and E5b at 1207.14
MHz. Users may receive signals from the two frequency bands independently.
1.3.4
Public Regulated Service
The PRS will be a restricted access service, offered to government agencies that require a high availability
navigation signal. The PRS service will utilize ranging codes that are encrypted with a highly secure
government encryption scheme. To enhance availability, the PRS service is intended to have anti-jamming and
anti-spoofing capabilities.
The PRS will be transmitted in two frequency bands – L1 at 1575.42 MHz, and E6 at 1278.75 MHz. Users may
receive signals from the two frequency bands independently.
1.3.5
Search and Rescue Service
A specific public service designed to assist in search and rescue operations will make it possible to locate
person and vehicles in distress. The vehicles will be fitted with beacons, which having been activated in the
event of an emergency will send an alerting signal to the rescue centre.
The Galileo Program provides this search and rescue service for users based on humanitarian and public
service principles of the international COSPAS-SARSAT system while at the same time making search and
rescue operations more effective.
1.4 EuroPak-15a Enclosure
The EuroPak-15a provides a hardware interface between your equipment and the NovAtel Euro-L1E5a card.
Each is a rugged, sealed enclosure that provides protection against adverse environments. It has DB-9
connectors to access data and status signals.
The EuroPak-15a offers the following features:
•
•
A mounting enclosure with a PCB interconnect back plane
Two serial ports provided on two DB-9P connectors (see the note below):
• COM1
• COM3 (the port is labelled COM2 on the enclosure but is COM3 in the software)
•
Auxiliary status and synchronization signals
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Chapter 1
Introduction
•
•
•
•
Antenna or signal generator Radio Frequency (RF) ports
Input power port
Indicators to provide power and communication status
An external oscillator port (input only)
The following accessories are included with the EuroPak-15a:
•
•
•
•
•
1 12V power adapter cable
1 I/O cable
1 null modem serial cable
1 straight through serial cable
A CD containing NovAtel’s PC utilities and product documentation
For technical specifications on the EuroPak-15a, please see Appendix A, Technical Specifications starting on
Figure 2: EuroPak-15a Enclosure
ꢀ The port labelled COM2 on the back of the receiver, see Figure 2 above, connects to COM3 of the internal
Euro-L1E5a card.
1.5 EuroPak-15a Features
The EuroPak-15a has been designed with the following features:
•
•
•
•
16 channel parallel tracking
Fully field-upgradeable firmware
Low power consumption
1 Hz raw data and position output rates
At a minimum, the following channel configuration is available:
•
•
•
•
•
8 GPS L1 (for L1L5GPS model)
8 GPS L5 (for L1L5GPS model)
5 Galileo L1 (for L1E5aGAL model)
5 Galileo E5a (for L1E5aGAL model)
6 GPS L1 (for L1E5aGAL model)
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Introduction
Additional features for the receiver card include:
Chapter 1
•
•
•
•
•
•
•
•
GEO signal processing
GPS signal processing
Galileo signal processing
Digital pulse blanking for the L1 signal
Digital pulse blanking for the L5 signal
Digital pulse blanking for the Galileo L1 signal
Digital pulse blanking for the Galileo E5a signal
A variant of the product, the EuroPak-15aT, is available. This variant contains a highly stable
OCXO frequency reference. The EuroPak-15aT can distribute this 10 MHz frequency reference
from its OSC port.
ꢀ Galileo signal processing will only be available on activated models.
Some of these features are discussed further in the following sections.
1.5.1
GEO Signal Processing
Specific channels have the capability to receive and process the SBAS signal provided by GEOs. These signals
are in-band at L1 and L5. They are identified through the use of SBAS-specific PRN numbers. The SBAS
message is decoded and separated into its various components. The SBAS message and associated
pseudorange are provided as an output.
1.5.2
Digital Pulse Blanking
Digital pulse blanking involves removing or attenuating pulses in the RF signal that exceed a specified level.
The EuroPak-15a provides digital pulse blanking for the GPS L1, GPS L5 signal, Galileo L1 and Galileo E5a
signal paths. Digital pulse blanking reduces the negative effects of pulsed interference.
Use the PULSEBLANKING command to enable/disable pulse blanking or control its sensitivity, see Page 62.
1.6 Functional Overview
In addition to the EuroPak-15a, an GNSS receiver system typically contains three other major components:
•
•
•
An antenna (and optional LNA power supply) or signal generator
A power supply
Data communications equipment
1.7 Internal Euro-L1E5a Card
The internal Euro-L1E5a card consists of a radio frequency and a digital electronics section.
1.7.1
Radio Frequency Section
The receiver obtains a filtered and amplified L1, L5 or E5a signal from the antenna or signal generator via the
coaxial cable. The RF section performs the translation from the incoming RF signal to an IF signal usable by
the digital section. It also supplies power to the active antenna’s LNA through the coaxial cable while
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Chapter 1
Introduction
maintaining isolation between the DC and RF paths. The RF section can reject a high level of potential
interference (for example, MSAT, Inmarsat, cellular phone, and TV sub-harmonic signals).
1.7.2
Digital Electronics Section
The digital section of the receiver receives a down-converted, amplified GNSS signal which it digitizes and
processes to obtain a navigation solution (position, velocity and time). The digital section consists of an analog-
to-digital converter, a 32-bit system processor, memory, control and configuration logic, signal processing
circuitry, serial peripheral devices, and supporting circuitry.
The digital section performs the translations and calculations necessary to convert the IF analog signals into
usable position and status information. It also handles all I/O functions, including the auxiliary strobe signals,
which are described in detail in Section 2.3.1 on Page 26. For input and output levels please see Appendix A,
1.8 Antenna or Signal Generator
The purpose of the antenna is to convert the electromagnetic waves transmitted by the satellites into RF signals.
An active antenna or a signal generator is required for the receiver to function properly.
Power for an antenna LNA is supplied by the receiver.
1.9 Principal Power Supply
A single external power supply capable of delivering 15 W is necessary to operate the receiver. See Appendix
WARNING: If the voltage supplied is below the minimum specification, the receiver will suspend
operation. If the voltage supplied is above the maximum specification, the receiver may
be permanently damaged, voiding your warranty.
1.10 Data Communications Equipment
A PC or other data communications equipment is necessary to communicate with the receiver and, if desired, to
store data generated by the receiver.
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Chapter 2
Installation
This chapter contains instructions and tips to set up your NovAtel receiver to create a GNSS receiver system.
At the time of publication, it is recommended that the L5 signal for the receiver be generated by a signal
generator as there are no L5 signals in space.
2.1 Additional Equipment Required
In order for the receiver to perform optimally, the following additional equipment is required:
•
•
•
•
•
•
•
An interface for power, communications, and other signals
An antenna or signal generator
A quality coaxial cable (and interconnect adapter cable as necessary)
Data communications equipment capable of serial communications
A serial cable (if not included with the receiver)
A power supply
A power cable (if not included with the receiver)
CAUTION:When the EuroPak-15a receiver is installed in a permanent location, such as in a
building, it should be protected by a lightening protection device according to local
2.1.1
Selecting an Antenna or Signal Generator
An L5 Signal Generator is available from NovAtel, see the Aviation Group’s contact information on Page 14 to
learn more.
The GPS-704-X antenna is a wide band passive antenna available from NovAtel. It is designed to operate in the
frequency range 1150-1650 MHz. An external LNA is required.
NovAtel offers a variety of antenna models. Each offer exceptional phase-center stability, a significant measure
of immunity against multipath interference and has an environmentally-sealed radome.
ꢀ Connection at the time of publication is directly to a signal generator. There are no L5 signals in space at
the present time.
2.1.2
Choosing a Coaxial Cable
An appropriate coaxial cable is one that is matched to the impedance of the antenna or signal generator and
receiver being used (50 ohms), and whose line loss does not exceed 10.0 dB. If the limit is exceeded, excessive
signal degradation will occur and the receiver may not be able to meet its performance specifications. NovAtel
offers a variety of coaxial cables to meet your interconnection requirements, including:
•
5, 15, or 30 m RF cables with TNC male connectors on both ends (NovAtel part numbers C006, C016
and C032 respectively)
Your local NovAtel dealer can advise you about your specific configuration. Should your application require
the use of cable longer than 30 m you will find the application note RF Equipment Selection and Installation at
High-quality coaxial cables should be used because a mismatch in impedance, possible with lower quality
cable, produces reflections in the cable that increase signal loss. Though it is possible to use other high-quality
RF cables, the performance specifications of the EuroPak-15a receivers are warranted only when used with
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Chapter 2
NovAtel-supplied accessories.
Installation
2.1.3
Power Supply Requirements
This section contains information on the requirements for the input power to the receiver. See Appendix A,
WARNING: If the voltage supplied is below the minimum specification, the receiver will suspend
operation. If the voltage supplied is above the maximum specification, the receiver may
be permanently damaged, voiding your warranty.
The receiver is designed to prevent internal damage when subjected to a reverse polarity power connection. It
also provides protection from short over voltage events. It is recommended that appropriate fuses or current
limiting be incorporated as a safety precaution on all power lines used. Use a sufficient gauge of wire to ensure
that the voltage at the connector is within the receiver’s requirements.
2.1.3.1
EuroPak-15a Enclosure
The EuroPak-15a is supplied with a 12 V power adapter with a built-in slow-blow fuse for use with a standard
12 VDC power outlet.
If a different supply is desired, the input range required is +9 to +18 VDC. The type of connector required to
mate with the receiver’s power connector is a 4-pin LEMO socket connector labelled PWR. The supply should
be capable of 15 W. See Appendix D, Replacement Parts starting on Page 126 for the LEMO connector part
number.
2.2 Installation Overview
Once you have selected the appropriate equipment, complete the following steps to set up and begin using your
NovAtel receiver.
1. Mount the antenna or signal generator to a secure, stable structure, see Section 2.2.1 on Page 25.
2. Connect the antenna or signal generator to the receiver with an RF cable, using the information
4. Connect the receiver to a PC or other data communications equipment by following the
Figure 3 on the next page shows a typical set up for an enclosed receiver.
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Installation
Chapter 2
1
2
5
4
7
6
Figure 3: Typical Receiver Installation
Reference
Description
1
2
3
4
5
6
7
Receiver
Antenna or Signal Generator
RF Cable
12V Power Cable
12V Power Cable with Optional AC Adapter or Aircraft Power Conditioner
Null Modem Data Cable
Data Communications Equipment
2.2.1
Mounting the Antenna or Signal Generator
When installing an antenna or signal generator system:
•
Mount the antenna on a secure, stable structure capable of safe operation in the specific
environment
Also, if mounting an antenna:
•
Choose an antenna location that has a clear view of the sky so that each satellite above the horizon
can be tracked without obstruction
2.2.2
Connecting the Antenna or Signal Generator to the Receiver
Connect the antenna or signal generator to the receiver using high-quality coaxial cable, as discussed in Section
The EuroPak-15a provides a TNC female connector, which can be connected to the antenna or signal generator
directly with any of NovAtel’s coaxial cables.
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Chapter 2
Installation
2.2.3
Applying Power to the Receiver
Connect the power supply to the PWR port of the EuroPak-15a receiver.
2.2.4
Connecting Data Communications Equipment
In order to communicate with the receiver by sending commands and obtaining logs, a connection to some
form of data communications equipment is required. The default configuration available for each of the
receiver types is given in the table below. Consult NovAtel Customer Service for more details on factory
configuration. See Appendix A, Technical Specifications starting on Page 110 for data connection details.
Table 1: Default Serial Port Configurations
Receiver
COM1
COM2
EuroPak-15a
RS-232
RS-232
Each port supports some, or all, of the following signals:
•
•
•
•
Clear To Send (CTS)
Transmitted Data (TXD)
Request To Send (RTS)
Received Data (RXD)
The EuroPak-15a enclosure is Data Terminal Equipment (DTE) so that TXD and RTS are outputs while RXD
and CTS are inputs. A null modem cable is required to connect to another DTE like a terminal or a PC.
2.3 Additional Features and Information
This section contains information on the additional features of the EuroPak-15a receivers, which may affect the
overall design of your receiver system.
2.3.1
Strobes
A set of inputs and outputs that provide status and synchronization signals are given on the EuroPak-15a. These
signals are referred to as strobes. As shown in Table 2 on Page 27, not all strobe signals are provided on all
receivers. However, for those products for which strobes are available, you may want to design your
installation to include support for these signals.
The EuroPak-15a enclosure provides strobe signals at its I/O port, as described in Table 54 on Page 114.
Strobe signals include an input and several outputs as described below:
•
•
•
Mark Input (Event1)
A pulse on this input triggers certain logs to be generated.
Falling edge is synchronized with internal GPS
measurements.
A pulse for which the falling edge is synchronized with GPS
time.
Measure Output (MSR)
Pulse Per Second Output (PPS)
•
•
Position Valid Output (PV)
Error Output (ERROR)
High when good GPS position and time solution.
High when a receiver hardware failure is detected.
See Appendix A, Technical Specifications starting on Page 110, for further information on the strobe signal
characteristics.
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Installation
Chapter 2
Table 2: Available Strobe Signals on the EuroPak-15a
STATUS STATUS
ERROR
Signal
EVENT1
MSR
PPS
PV
_RED
_GREEN
EuroPak-15a
I/O port,
pin 4
I/O port, I/O port, I/O port, I/O port, Not
pin 3 pin 2 pin 5 pin 8 available
Not
available
ꢀ The ground return pin for these signals is Pin 9.
2.3.2
Status Indicators
The EuroPak-15a receivers have LED indicators that provide the status of the receiver. The EuroPak-15a
Table 3: EuroPak-15a Status Indicators
Indicator
COM1
Indicator Color
Status
Green
Data is being transmitted from COM1
Red
Green
Red
Data is being received on COM1
Data is being transmitted from COM3
Data is being received on COM3
The receiver is powered
COM2
PWR
Red
2.3.3
External Oscillator
ꢀ You may connect an external oscillator to a EuroPak-15a model, without an internal oven-controlled
crystal oscillator (OCXO) as explained in this section. On the EuroPak-15aT model, the OSC port is for
output from the internal OCXO only, and therefore this section does not apply to it.
For certain applications requiring greater precision than what is possible using the on-board 20 MHz, voltage-
controlled, temperature-compensated crystal oscillator (VCTCXO), you may wish to connect the EuroPak-15a
to an external, high-stability oscillator. The external oscillator can be either 5 MHz or 10 MHz.
DISABLED. This means the external clock input is off and the board is using the on-board VCTCXO.
Installation consists of connecting a cable from the external oscillator to the EuroPak-15a’s external oscillator
input connector.
The BNC external oscillator port, labelled OSC, is used for input signals on the EuroPak-15a and for output
issued to define the clock model (for example, cesium, rubidium or ovenized crystal). If the input clock rate is
5 MHz, the EXTERNALCLOCK command must be issued to change the 10 MHz default rate.
2.3.4
Mounting Bracket
Along with the EuroPak-15a enclosure, mounting kits have been provided to facilitate mounting the receivers
to a surface. To install the mounting bracket provided with the EuroPak-15a, refer to the instructions provided
ꢀ The mounting kits are not designed for use in high-dynamics/vibration environments. Contact NovAtel,
see Page 14, if your application requires the EuroPak-15a to be mounted in these types of environments.
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Chapter 3
Operation
Before operating the EuroPak-15a for the first time, ensure that you have followed the installation instructions
in Chapter 2. From here on, it will be assumed that testing and operation of the EuroPak-15a will be performed
while using a personal computer (PC), which allows the greatest ease and versatility.
3.1 Pre-Start Check List
Before turning on power to the EuroPak-15a, ensure that all of the following conditions have been met:
•
•
The antenna or signal generator is properly installed, powered, and connected
The PC is properly connected using a serial cable, and its communications protocol has been
configured to match that of the EuroPak-15a
Supply power to the EuroPak-15a only after all of the above checks have been made. Note that the warm-up
process may take several minutes, depending on ambient temperature.
3.2 Start-Up
The EuroPak-15a’s firmware resides in non-volatile memory. After supplying power to the unit, wait a moment
for self-boot, and the EuroPak-15a will be ready for command input.
The initial start-up indicator to let you know that the EuroPak-15a's main serial port is ready to communicate:
•
Your PC will display the following prompt, indicating you are connected through the COM1 port:
[COM1]
The receiver has 4 modes of operation including power-up mode:
•
•
•
•
Power-Up
Operational
Fault
Maintenance
The EuroPak-15a is in power-up mode after receiving a reset signal. While in this mode, everything is disabled
except for the clock generators and microprocessor interface. During this mode, Firmware (FW) is transferred
from Flash to RAM, the 32-bit CRC is verified on the FW load and the Initiated Built In Test (IBIT) is
exercised to determine whether the receiver is usable. This mode ends when the functional blocks of the
receiver have been enabled, initialized and the IBIT has been successfully executed.
The EuroPak-15a is in operational mode following power-up mode and before a fault is discovered by the
Continuous Built In Test (CBIT) and goes into fault mode when the device outputs are affected by one or more
faults preventing its use.
The EuroPak-15a is in maintenance mode when it is loading firmware. Maintenance mode can only be entered
via the Power-up mode.
Once you are connected, commands can be entered as explained in Section 3.3, Communicating with the
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Operation
Chapter 3
3.3 Communicating with the EuroPak-15a
Communication with the receiver consists of issuing commands through the communication ports from an
external serial communications device. This could be either a PC or laptop that is directly connected to the
receiver serial port using a null modem cable.
The commands and logs used by the EuroPak-15a, as well as the fields within them, follow specific formats,
which are discussed in Chapter 4. The valid commands, which are used to control the operation and data
logging of the EuroPak-15a, are specified in Chapter 5. Chapter 6 provides details on the data logs that can be
requested from the EuroPak-15a. It is to your advantage to become thoroughly familiar with Chapters 4
3.4 Getting Started
Included with your receiver are NovAtel’s GPSolution (Aviation) and Convert programs. GPSolution
(Aviation) is a Microsoft Windows-based GUI which allows you to access the receiver's many features without
the need for communications protocol or to write special software. The Convert utility is a Windows-based
utility that allows you to convert between file formats, and strips unwanted records for data file compilation.
See the EuroPak-15a Quick Start Guide for more information on their installation.
ꢀ You must install the Aviation version of the PC Utilities provided on your CD. It is only this version,
GPSolution (Aviation), of GPSolution that works with the EuroPak-15a receiver.
3.4.1
Starting the Receiver
The receiver’s software resides in read-only memory. When first powered, it undergoes a complete self-test. If
an error condition is detected during a self-test, the self-test status word changes. This self-test status word can
be viewed in the header of any data output log. See also Chapter 8, Built-In Status Test starting on Page 107.
3.4.2
Communicating with the Receiver Using GPSolution (Aviation)
Launch the GPSolution (Aviation) program and select Device | Open from its main menu. The Open dialog
appears. The example below shows an Open dialog with a possible configurations already set up. Your
configurations may be different or you may have none at all. In that case, the Available device configs window
would be empty.
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Chapter 3
Operation
Refer to GPSolution (Aviation)’s Help file by selecting Help | Contents from the main menu to see Help for
windows and their descriptions. Ensure you can see the Console and ASCII Messages windows by selecting
them under View in the main menu.
When the receiver is first turned on, no data is transmitted from the COM ports except for the port prompt. The
Console window displays a port name:
[COM1] if connected to COM1 port,
or
[COM3] if connected to COM3 port
Any of the above prompts indicate that the receiver is ready and waiting for command input.
ꢀ If you find that GPSolution (Aviation) is unable to locate your EuroPak-15a receiver, it may be that you
have previously used the SAVECONFIG command. In this case, try using a different COM port to
communicate to the receiver. Once communication has been established, issue a FRESET STANDARD
command. You should now be able to use your original communication port again.
WARNING!:
Ensure all other windows are closed in GPSolution (Aviation) when entering the
SAVECONFIG command in the Console window.
Commands are typed at the interfacing computing device’s keypad or keyboard, and executed after issuing a
carriage return command which is usually the same as pressing the <Enter> key.
An example of a response to an input command is the FIX POSITION command. It can be entered like this:
[COM2] fix position 51.11635 -114.0383 1048.2 [carriage return]
<OK
where [COM2] is the port prompt, the bolded type is the command you enter from you keypad or
keyboard and [carriage return] indicates that you should press the <Enter> key.
The above example illustrates command input to the base receiver’s COM2 port which sets the position of the
base station receiver for differential operation. Confirmation that the command was actually accepted is the
appearance of <OK.
If a command is entered incorrectly, the receiver responds with:
<INVALID MESSAGE ID
(or a more detailed message)
WARNING!:
Ensure the Control Panel’s Power Settings on your PC are not set to go into Hibernate
or Standby modes. Data will be lost if one of these modes occurs during a logging session.
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Chapter 4
Using Commands and Logs
Chapter 5 and Chapter 6 provide the details of the commands and logs used to communicate with the EuroPak-
15a. The sections below give information on using these messages, including the formats they can take and the
responses they may provide.
4.1 Entering Commands
The EuroPak-15a is capable of responding to many different input commands. The commands offer a wide
range of flexibility and can be used to control the following:
•
•
•
The overall status of the EuroPak-15a
Input and output functions
Configuration of a specific channel of the EuroPak-15a
The following rules apply when entering commands and logs:
1. You must enter commands in Abbreviated ASCII format. The name of the command and its
parameters are entered.
2. The commands are not case sensitive. For example:
FIX POSITION or fix position
3. At the end of a command or command string, press <ENTER>.
4.1.1
Command Settings on Power-Up
When the receiver is first powered up, or after an FRESET command, all commands revert to the factory
default settings.
ꢀ The FRESET command causes all previously stored information saved to non-volatile memory to be
4.1.1.1
Factory Defaults
The factory defaults for the EuroPak-15aT timing model are:
ANTENNAPOWER ON
CLOCKADJUST DISABLE
COM COM1 9600 N 8 1 N OFF ON
COM COM3 115200 N 8 1 N OFF ON
POSITIONTYPE GPSL1
SDLLBW n 0.2
where n is for channel numbers 0 to 15 inclusive
where n is for channel numbers 0 to 15 inclusive
SPLLBW n 3.0
EXTERNALCLOCK OCXO 10 MHZ
The factory defaults for the EuroPak-15a non-timing model are:
ANTENNAPOWER ON
CLOCKADJUST ENABLE
COM COM1 9600 N 8 1 N OFF ON
COM COM3 115200 N 8 1 N OFF ON
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Chapter 4
POSITIONTYPE GPSL1
Using Commands and Logs
SDLLBW n 0.2
where n is for channel numbers 0 to 15 inclusive
where n is for channel numbers 0 to 15 inclusive
SPLLBW n 15.0
EXTERNALCLOCK DISABLE
4.1.1.2
Default Thresholds
For L1 GPS, L1 WAAS and L1 Galileo, the acquistion threshold is 38 dB-Hz, the tracking threhold is 22 dB-Hz
and the cross-correlation threshold is 36 dB-Hz.
For L5 GPS, L5 WAAS and E5a Galileo, the acquistion threshold is 36 dB-Hz, the tracking threhold is 22 dB-
Hz and the cross-correlation threshold is 36 dB-Hz.
4.1.1.3
Default AGC Modes
The AGC modes are set to AUTO by default for all frequencies.
4.1.2
Determining the Current Command Settings
To determine the current command settings of a receiver, request an RXCOMMANDS log, which is described in
Section 6.3.8 on Page 88. This will provide a listing of all commands and their parameter settings. This log
provides the most complete information on receiver configuration.
For some commands, including COM and LOG, multiple parameter sets can exist. For example, the LOG
command can be entered with one set of parameters to enable logging of the PSRPOS log. It can then be
entered again with a second set of parameters to configure the EuroPak-15a to capture the RANGE log. When
the LOG command is entered the second time, the new parameter set does not overwrite the first, it exists in
addition to the first set.
4.1.3
Response Formats
The format of the response is dependent on the format of the input command. If the command is input as
Abbreviated ASCII, the output will be Abbreviated ASCII.
The Abbreviated ASCII response consists of a leading < followed by the response string, like the example
below:
<OK
4.1.4
Response Messages
The receiver is capable of outputting several responses for various conditions. Most of these responses are error
messages to indicate when something is not correct. Table 4 on Page 33 outlines the various response strings
and message IDs.
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Chapter 4
Table 4: Response Messages
ID
String
Meaning
OK
1
3
Command was received correctly
NOT ENOUGH RESOURCES IN
SYSTEM
The request has exceeded a limit (for example, the
maximum number of logs are being generated)
DATA PACKET DOESN’T VERIFY
COMMAND FAILED ON RECEIVER
INVALID MESSAGE ID
4
5
6
7
9
Data packet is not verified
Command did not succeed in accomplishing requested task
The input message ID is not valid
INVALID MESSAGE FIELD = X
MESSAGE MISSING FIELD
Field x of the input message is not correct
A field is missing from the input message
ARRAY SIZE FOR FIELD X EXCEEDS
MAX
10
Field x contains more array elements than allowed
PARAMETER X IS OUT OF RANGE
11
14
Field x of the input message is outside the acceptable limits
TRIGGER X NOT VALID FOR THIS LOG
Input trigger x is not valid for this type of log
NO VALID AUTH CODE FOR THAT
MODEL
19
The model attached to the authcode is not valid
CHANNEL IS INVALID
20
21
23
24
25
26
27
31
33
The channel number is not correct
The requested rate is invalid
Channels are locked due to error
Injected time is invalid
REQUESTED RATE IS INVALID
CHANNELS LOCKED DUE TO ERROR
INJECTED TIME INVALID
COM PORT NOT SUPPORTED
MESSAGE IS INCORRECT
INVALID PRN
The COM port is not supported
The message is invalid
The PRN is invalid
MESSAGE TIMED OUT
The message has timed out
Unknown COM port requested
UNKNOWN COM PORT REQUESTED
HEX STRING NOT FORMATTED
CORRECTLY
34
35
36
Hex string not formatted correctly
The baud rate is invalid
INVALID BAUD RATE
MESSAGE IS INVALID FOR THIS
MODEL
This message is invalid for this model of receiver
COMMAND ONLY VALID IF IN NVM
FAIL MODE
40
41
78
Command is only valid if NVM is in fail mode
The offset is invalid
INVALID OFFSET
MAX NUMBER OF USER MESSAGES
REACHED
The maximum number of user messages allowed has been
reached
GPS PRECISE TIME IS ALREADY
KNOWN
84
GPS precise time is already known
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Chapter 4
Using Commands and Logs
4.2 Logging Data
You can control how the EuroPak-15a logs data by using the LOG command given on Page 59. A field within
this command allows you to specify which data log from Chapter 6 to capture. Note the following however:
1. The EuroPak-15a can handle 20 logs at a time. If you attempt to log more than 20 logs at a time,
the receiver will respond with the error message:
Not enough resources in system
2. Maximum flexibility for logging data is provided to you by these logs. You are cautioned,
however, to recognize that each log requested requires additional CPU time and memory buffer
space. Too many logs may result in lost data and degraded CPU performance. Receiver overload
can be monitored using the idle-time field and the buffer overrun bits of the Receiver Status field,
which are both found in any log header.
When a log is generated, it is sent to the serial port specified by the portparameter in the entered LOG
command.
4.2.1
Log Types
The receiver is capable of generating many different logs. These logs are divided into the following three types:
•
•
Synchronous
The data contained in synchronous logs is generated on a regular schedule.
Asynchronous
The data in asynchronous logs is generated at irregular intervals. If these logs
were collected on a regular schedule, there would be a delay in capturing the
new data. The result is that changes to the data are not captured the moment
they were available.
•
Polled
The data in polled logs is generated only when requested. Typically the data
in these logs, such as configuration settings, does not change.
4.2.2
Log Triggers
Each log can be configured for output when a certain condition, or trigger, is met. The possible triggers are:
•
•
•
•
ONNEW
Output a new log whenever the message is updated (not necessarily changed).
Output a new log whenever the message has changed.
ONCHANGED
ONTIME
ONCE
Output a new log at a specified interval (in seconds).
Output the current, existing message. Only a single log will be generated.
For each log type described in Section 4.2.1, Log Types only certain triggers are valid. For example, the
VERSION log is a polled log because it does not change. Therefore, it would not make sense to log this kind of
Table 5: Log Triggers for Each Log Type
Type
Recommended Triggers
Illegal Triggers
ONNEW
ONCHANGED
Synchronous
Asynchronous
Polled
ONTIME
ONCHANGED
ONCE
-
ONNEW
ONCHANGED
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Chapter 4
4.2.3
Specifying Log Formats
When entering the LOG command using ASCII format, the default format for the output log is ASCII. To
generate logs in a different format, a suffix is added to the name of the message being requested. To request a
log in ASCII format, add Ato the end of the log as shown below.
LOG ALMANACA
To request a log in Binary format, Bis added to the end of the log name.
LOG RANGEB ONTIME 30
When issuing Binary logs, the output message type is set in the Message Type field in the command header, as
4.3 Log Formats
The receiver handles all incoming and outgoing NovAtel logs using two different formats:
•
•
ASCII
Binary
This allows for some versatility in the way the EuroPak-15a can be used.
4.3.1
ASCII
The ASCII format is readable by both you and a computer. The structures of all ASCII messages follow the
general conventions as noted here:
1. Basic format:
#HEADER_PARAMS;PARAM_1,PARAM_2,...,PARAM_N*XXXXXXXX[CR][LF]
2. The lead code identifier for each record is '#'. This identifier is followed by the header parameters,
3. Each log is of variable length depending on the amount of data and field formats.
4. All data fields are delimited by a comma ',' with two exceptions. The first exception is the last
header field which is followed by a ';' to denote the start of the data message. The other exception
is the last data field, which is followed by a '*' to indicate end of message data.
5. Each log ends with a hexadecimal number preceded by an asterisk and followed by a line
termination using the carriage return and line feed characters, for example,
*1234ABCD[CR][LF]. This value is a 32-bit cyclic redundancy check (CRC) of all bytes in the
message, excluding the '#' identifier and the asterisk preceding the checksum digits. See Section
6. An ASCII string is one field and is surrounded by double quotation marks, for example, “ASCII
string”. If separators are surrounded by quotation marks then the string is still one field and the
separator will be ignored, for example, “xxx,xxx”is one field. Double quotation marks within a
string are not allowed.
7. If the receiver detects an error parsing an input message, it will return an error response message.
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Chapter 4
The ASCII message header is formatted as follows:
Using Commands and Logs
Table 6: ASCII Message Header Structure
Description
Field
Name
Field
Type
Ignored
on Input
Field
Sync character. The ASCII message is always preceded by a
1
2
3
sync
Char
Char
Char
N
N
Y
single ‘#’ symbol.
The ASCII name of the message. The names of logs are given
message
port
The name of the port from which the log was generated.
4
5
Reserved
idle time
ULong Reserved for internal use
Float The minimum percentage of time that the processor is idle
N
Y
The quality of the GPS time, as described in Section 4.4.2.4
6
7
8
time status Enum
Y
Y
Y
week
ULong GPS week number
Seconds from the beginning of the GPS week accurate to the
millisecond level
seconds
GPSec
An eight digit hexadecimal number representing the status of
receiver
status
9
ULong various hardware and firmware components of the receiver.
Y
10
11
12
ULong
Y
Y
N
Reserved
;
Reserved for internal use
ULong
Char
The ‘;’ character indicates the end of the header
Example ASCII Format Log:
#PSRPOSA,COM1,0,43.0,FINESTEERING,265,320943.000,00840000,
0000,33331;SOL_COMPUTED,SINGLE,51.11638529847,-114.03825624352,
1045.2359,0.0000,WGS84,1.5908,1.4096,2.3924,"",0.000,0.000,10,8,
0,0,0,0,0,0*84ea7b68[CR][LF]
4.3.2
Binary
Binary messages are meant strictly as a machine readable format. They are also ideal for applications where the
amount of data being transmitted is fairly high. Because of the inherent compactness of binary as opposed to
ASCII data, the messages are much smaller. This allows a larger amount of data to be transmitted and received
by the receiver’s communication ports. The structure of all Binary format messages follows the general
conventions as noted here:
1. Basic format:
Header
3 sync bytes plus 25 bytes of header information. The header length is variable
as fields may be appended in the future. Always check the header length.
Parameters Variable length binary data
CRC 4 bytes
2. The 3 Sync bytes are always:
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Chapter 4
Byte
First
Hex
AA
44
Decimal
170
Second
Third
68
12
18
3. The CRC is a 32-bit cyclic redundancy check performed on all data including the header. See
Table 7: Binary Message Header Structure
Field
Name
Field
Type
Binary Binary Ignored
Bytes Offset on Input
Field
Description
Hexadecimal 0xAA
1
2
3
sync
Char
1
1
1
0
1
2
N
N
N
sync
sync
Char
Char
Hexadecimal 0x44
Hexadecimal 0x12
header
length
4
UChar Length of the header
1
3
N
message
ID
Message ID. The message IDs for logs are given in
5
UShort
2
4
N
message
type
Message type indicator, as explained in Section
6
7
8
Char
1
1
2
6
7
8
N
N
N
The port from which the log was generated.
port
address
Char
message
length
The length in bytes of the body of the message. This
does not include the header nor the CRC.
UShort
For multiple related logs. A number that counts
down from N-1 to 0 where N is the number of
UShort related logs and 0 means it is the last one of the set.
Most logs only come out one at a time in which case
this number is 0.
9
sequence
idle time
2
1
10
12
N
Y
The percentage of time that the processor is idle in
the last second. Take the time (0-200) and divide by
two to give the percentage of time (0-100%).
10
Char
The quality of the GPS time, as described in Section
a
b
11
12
13
time status Enum
13
14
16
1
N
N
N
b
b
week
UShort GPS week number
2
4
milli-
seconds
GPSec Milliseconds from the beginning of the GPS week
32 bits representing the status of various hardware
ULong and firmware components of the receiver. This
receiver
status
14
4
20
Y
15
16
UShort
2
2
24
26
Y
Y
Reserved
Reserved for internal use
UShort
a. This ENUM is not 4 bytes long but, as indicated in the table, is only 1 byte.
b. These time fields are ignored if Field #11, Time Status, is invalid. In this case the current receiver time is used. The
recommended values for the three time fields are 0, 0, 0.
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Chapter 4
Using Commands and Logs
4.4 Fields
The commands and logs for the EuroPak-15a use a variety of field types to convey data. The following sections
provide information on the types of fields used and some of the more commonly-used fields.
4.4.1
Field Types
The following table describes the field types used in the commands and logs.
Table 8: Field Types
Binary Size
Type
Description
(Bytes)
An 8-bit signed integer in the range -128 to +127. This integer value may
be the ASCII code corresponding to the specified character. In ASCII or
Abbreviated ASCII this comes out as an actual character.
Char
1
An 8-bit unsigned integer. Values are in the range from +0 to +255. In
ASCII or Abbreviated ASCII this comes out as a number.
UChar
1
Short
2
2
4
4
A 16-bit signed integer in the range -32768 to +32767.
A 16-bit unsigned integer in the range +0 to +65535.
UShort
Long
A 32-bit signed integer in the range -2147483648 to +2147483647.
A 32-bit unsigned integer in the range +0 to +4294967295.
ULong
64 bits, with 1 for the sign, 11 for the exponent, and 52 for the mantissa.
Its range is ±1.7E308 with at least 15 digits of precision. This is IEEE
754.
Double
Float
8
4
4
32 bits, with 1 for the sign, 8 for the exponent, and 23 for the mantissa.
Its range is ±3.4E38 with at least 7 digits of precision. This is IEEE 754.
A 4-byte enumerated type beginning at zero (an unsigned long). In
Binary, the enumerated value is output. In ASCII or Abbreviated ASCII,
the enumeration label is spelled out.
Enum
Two separate formats that depend on whether the output is requested in
Binary or an ASCII format. For Binary the output is in milliseconds and
is a long type. For ASCII the output is in seconds and is a float type.
GPSec
Hex
4
n
n
A packed, fixed length (n) array of bytes in Binary but in ASCII or
Abbreviated ASCII is converted into 2 character hexadecimal pairs.
A variable length array of bytes that is null-terminated in the Binary case.
The maximum byte length for the field is shown in the row in the log or
command table.
String
Section 9 on Page 39 shows the arrangement of bytes within each field type when used by IBM PC computers.
All data sent to or from the receiver, however, is read Least Significant Bit (LSB) first, opposite to what is
shown in Table 9. Data is then stored in the receiver LSB first. For example, in char type data, the LSB is bit 0
and the Most Significant Bit (MSB) is bit 7.
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Chapter 4
Table 9: Byte Arrangements
7
0
char
address n
15
7
0
short
long
n + 1 address n
31 23
15
7
0
tw o's compliment
n + 3
63 62
Biased Exponent|
n + 7 n + 6
31 30 23 22
Biased Exponent| 23-bits mantissa
n + 3 n + 2 n + 1 address n
n + 2
n + 1 address n
52 51
0
double
S
52-bits mantissa
n + 4 n + 3
n + 5
n + 2
n + 1 address n
0
float
S
4.4.2
Commonly-Used Fields
Some of the more commonly-used fields are discussed in this section.
4.4.2.1
Serial Port Identifiers
The values used to indicate serial ports are given below.
Table 10: Serial Port Identifier Values
ASCII
COM1
COM3
Binary
32
96
4.4.2.2
Message Type Indicator
The Message Type Indicator is a byte given in numerous binary format messages and all binary headers. It
Table 11: Message Type Byte Format
Bit
Description
0-4
Reserved
Message format, where
00 = Binary
5-6
7
01 = ASCII
10 = Abbreviated ASCII, NMEA
11 = Reserved
Response indicator, where
0 = original message
1 = response message.
information on logging data.)
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Chapter 4
Using Commands and Logs
4.4.2.3
Message Time Stamps
All NovAtel format messages generated by the receiver have a GPS time stamp in their header. GPS time is
referenced to UTC with zero point defined as midnight on the night of January 6, 1980 at 0:00 hours. The time
stamp consists of the number of weeks since that zero point, the EuroPak-15a rolls over, (0 to 1023) and the
number of seconds since the last week number change (0 to 603,799). GPS time differs from UTC time since
leap seconds are occasionally inserted into UTC but GPS time is continuous. In addition a small error (less than
1 microsecond) can exist in synchronization between UTC and GPS time. The TIME log reports both GPS and
UTC time and the offset between the two.
The data in synchronous logs, like the RANGE log, are based on a periodic measurement of satellite
pseudoranges. The time stamp on these logs is the receiver estimate of GPS time at the time of the
measurement. When setting time in external equipment, a small synchronous log with a high baud rate will be
accurate to a fraction of a second. A synchronous log with trigger ONTIME 1can be used in conjunction with
the 1 PPS signal to provide relative accuracy better than 250 ns.
Other log types (asynchronous and polled) are triggered by an external event and the time in the header may not
be synchronized to the current GPS time. Logs that contain satellite broadcast data have the transmit time of
their last subframe in the header. In the header of differential time matched logs, the time of the matched
reference and local observation that they are based on is given. Logs triggered by a mark event have the
estimated GPS time of the mark event in their header. The header of a polled log, like VERSION, gives the
approximate GPS time when its data was generated.
4.4.2.4
GPS Time Status
All reported receiver times are subject to a qualifying time status. This status gives you an indication of how
Table 12: GPS Time Status
GPS Time Status
(Decimal)
GPS Time Status
(ASCII)
Description
20
UNKNOWN
Time validity is unknown.
60
APPROXIMATE
COARSE
Time is set approximately.
100
120
This time is valid to coarse precision.
Time is coarse set, and is being steered.
COARSESTEERING
Position is lost, and the range bias cannot be
calculated.
130
FREEWHEELING
160
180
FINE
Time has fine precision.
FINESTEERING
Time is fine, set and is being steered.
Time from satellite. This is only used in logs
containing satellite data such as ephemeris
and almanac.
200
SATTIME
There are several distinct states that the receiver will go through:
•
•
•
•
UNKNOWN
COARSE
FREEWHEELING
FINE/FINESTEERING
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Chapter 4
On start up, and before any satellites are being tracked, the receiver can not possibly know the current time. As
such, the receiver time starts counting at GPS week 0 and second 0.0. The time status flag is set to
UNKNOWN.
After the first ephemeris is decoded, the receiver time is set to a resolution of ±10 milliseconds. This state is
qualified by the COARSE or COARSESTEERING time status flag depending on the state of the
CLOCKADJUST switch.
Once a position is known and range biases are being calculated, the internal clock model begins modelling the
position range biases and the receiver clock offset.
Modelling continues until the model is a good estimation of the actual receiver clock behavior. At this time, the
receiver time is adjusted again, this time to an accuracy of ±1 microsecond. This state is qualified by the FINE
time status flag.
The final logical time status flag depends on whether CLOCKADJUST is enabled or not, see Page 50. If
CLOCKADJUST is disabled, the time status flag never improves on FINE. The time is only adjusted again to
within ±1 microsecond if the range bias gets larger than ±250 milliseconds. If CLOCKADJUST is enabled, the
time status flag is set to FINESTEERING and the receiver time is continuously updated (steered) to minimize
the receiver range bias.
If for some reason position is lost and the range bias cannot be calculated, the time status is degraded to
FREEWHEELING.
4.4.2.5
32-Bit CRC
The ASCII and Binary message formats all contain a 32-bit Cyclic Redundancy Check (CRC) for data
verification. This allows you to ensure that the data received (or transmitted) is valid with a high level of
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Chapter 4
#define CRC32_POLYNOMIAL 0xEDB88320L
Using Commands and Logs
/* --------------------------------------------------------------------------
Calculate a CRC value to be used by CRC calculation functions.
-------------------------------------------------------------------------- */
unsigned long CRC32Value(int i)
{
int j;
unsigned long ulCRC;
ulCRC = i;
for ( j = 8 ; j > 0; j-- )
{
if ( ulCRC & 1 )
ulCRC = ( ulCRC >> 1 ) ^ CRC32_POLYNOMIAL;
else
ulCRC >>= 1;
}
return ulCRC;
}
/* --------------------------------------------------------------------------
Calculates the CRC-32 of a block of data all at once
-------------------------------------------------------------------------- */
unsigned long CalculateBlockCRC32(
unsigned long ulCount,
/* Number of bytes in the data block */
unsigned char *ucBuffer ) /* Data block */
{
unsigned long ulTemp1;
unsigned long ulTemp2;
unsigned long ulCRC = 0;
while ( ulCount-- != 0 )
{
ulTemp1 = ( ulCRC >> 8 ) & 0x00FFFFFFL;
ulTemp2 = CRC32Value( ((int) ulCRC ^ *ucBuffer++ ) & 0xff );
ulCRC = ulTemp1 ^ ulTemp2;
}
return( ulCRC );
}
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Chapter 5
Commands
5.1 Functional Listing of Commands
Table 13 lists the commands by function. Please see Section 5.3 on Page 45 for a more detailed description of
each individual command.
Table 13: Commands By Function
Command
Description
COMMUNICATIONS, CONTROL AND STATUS
Set serial port configuration
COM
LOG
Request a log
UNLOG
Remove a specified log from logging control
Remove all logs from logging control
UNLOGALL
GENERAL RECEIVER CONTROL
Control Automatic Gain Control (AGC) functionality
Configure receiver’s DLL filter bandwidth
Configure receiver’s phase-lock-loop bandwidths
Perform a hardware reset
AGCMODE
SDLLBW
SPLLBW
RESET
FRESET
Reset receiver to factory default
POSITION CONTROL
FIX
Constrain receiver position
POSITIONTYPE
Control the position solution on GPS L1 or L5 signals
SATELLITE TRACKING AND CHANNEL CONTROL
Assign individual satellite channel
ASSIGN
CHANCONFIG
ECUTOFF
Set receiver channel tracking configuration
Set satellite elevation cut-off angle
PULSEBLANKING
STHRESHOLD
UNASSIGN
Enable/disable digital pulse blanking for L1 Galileo or E5a signals
Control signal thresholds for acquisition, tracking and cross correlation
Unassign a previously ASSIGNed channel
CLOCK INFORMATION, STATUS, AND TIME
Enable or disable adjustments to the internal clock and 1PPS output
Set the parameters for an external clock
CLOCKADJUST
EXTERNALCLOCK
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Chapter 5
Commands
5.2 Command Summary
Table 14: Command Summary
Description
Message
Command Name
ID
Syntax
agcmode frequency mode
[pulsewidth loadvalue]
AGCMODE
ASSIGN
Control Automatic Gain Control (AGC)
Assign individual satellite channel to a PRN
229
27
assign channel [state] [prn
[Doppler window]]
chanconfig config
CHANCONFIG
CLOCKADJUST
Set receiver channel tracking configuration
Enable clock adjustments
501
15
clockadjust switch
com [port] bps [parity
[databits [stopbits
[handshake [echo [break]]]]]]
COM
Serial port configuration control
4
ecutoff angle
ECUTOFF
Set satellite elevation cutoffs
Set external clock parameters
Fix height, position or velocity
50
externalclock clocktype
[freq] [h0 [h1 [h2]]]
EXTERNALCLOCK
230
fix type [lat lon height]
FIX
44
20
Clear data stored in non-volatile memory. freset
FRESET
Followed by a receiver reset.
log [port] message [trigger]
[period [offset] [hold]]
LOG
Request logs from receiver
1
Set position filter to GPS L1 or L5
frequency
positiontype frequency
POSITIONTYPE
PULSEBLANKING
836
519
pulseblanking frequency
switch
Enables or disables digital pulse blanking
for L1 or L5 signals.
reset [delay]
RESET
18
Perform a hardware reset
sdllbw dsigchan bw
spllbw psigchan bw
SDLLBW
SPLLBW
Configure receiver’s DLL filter bandwidth
Configure receiver’s phase-lock-loop bw
800
801
sthreshold sigchan acqui
lock crosscorr
Control signal thresholds for acquisition,
tracking and cross correlation
STHRESHOLD
803
unassign channel
unlog [port] datatype
unlogall [port]
UNASSIGN
UNLOG
Unassign a previously ASSIGNed channel
Remove log from logging control
29
36
38
UNLOGALL
Remove all logs from logging control
44
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Commands
Chapter 5
5.3 Command Reference
All syntax strings and command examples given in this section are in the Abbreviated ASCII format, unless
otherwise indicated. The tables provided show the fields necessary for all formats unless otherwise noted.
5.3.1
AGCMODE Control Automatic Gain Control
ꢀ 1. This command can fundamentally change the way that the receiver operates. Do not alter the default
settings unless you are confident that you understand the consequences.
2. When the AGC mode is disabled, the Receiver Status word in the message header, discussed in
the feedback loop is within 7.5% of the set point.
This command controls the EuroPak-15a’s Automatic Gain Control (AGC) mechanism, which has two primary
functions:
•
•
To perform the analog-to-digital conversions in the receiver’s front end.
Mitigate jamming.
Table 15: Frequency Values for AGCMODE Command
ASCII
L1
Description
a
L1 GPS and Galileo channels
a
L5
L5 GPS and E5a Galileo channels
a. Changing GPS L1 affects Galileo L1 and
changing GPS L5 affects Galileo E5a
Table 16: AGC Mode Values
ASCII
AUTO
Description
Specifies that the default pulse width
and load values should be used.
Specifies that the values specified in the
pulsewidth and loadvalue fields should
be used.
MANUAL
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Chapter 5
Syntax:
Commands
Message ID: 229
AGCMODE FREQUENCY MODE [ PULSEWIDTH LOADVALUE ]
Valid Values
Field
Binary Binary
Field
Description
Format
Name
Bytes
Offset
ASCII
Binary
1
2
header
H
0
Specifies which signal
type to apply the
command to.
frequency
mode
Enum
4
4
H
Specifies whether to
use the default or
custom values for the
pulse width and load
value.
3
H+4
Enum
Pulse width. A value is
only required when the
mode field is set to
MANUAL.
4
5
pulsewidth 35 to 262144
4
4
H+8
Float
Float
Modulus load value. A
value is only required
when the mode field is
set to MANUAL.
loadvalue
35 to 262144
H+12
Example:
AGCMODE L1 MANUAL 40 50
Table 17: Antispoofing Flag Values
ASCII
Description
FALSE
TRUE
Antispoofing is disabled.
Antispoofing is enabled.
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Commands
Chapter 5
5.3.2
ASSIGN Assign Individual Satellite Channels
ꢀ The ASSIGN command should only be used by advanced users.
This command may be used to aid in the initial acquisition of a satellite by allowing you to override the
automatic satellite/channel assignment and reacquisition processes with manual instructions. The command
specifies that the selected tracking channel should search for a specified satellite at a specified Doppler
frequency within a specified Doppler window.
The instruction will remain in effect for the specified SV channel and PRN, even if the assigned satellite
subsequently sets. If the satellite Doppler offset of the assigned SV channel exceeds that specified by the
window parameter of the ASSIGN command, the satellite may never be acquired or re-acquired. If a PRN has
been assigned to a channel and the channel is currently tracking that satellite, when the channel is set to AUTO
tracking, the channel will immediately idle and return to automatic mode.
To cancel the effects of ASSIGN, you must issue one of the following:
•
•
The ASSIGN command with the state set to AUTO
The UNASSIGN command
These will return SV channel control to the automatic search engine immediately.
ꢀ 1. Assigning a PRN to an SV channel does not remove the PRN from the search space of the automatic
searcher; only the SV channel is removed (i.e. the searcher may search and lock onto this PRN on
another channel). The automatic searcher only searches for PRNs 0 to 37 for GPS channels and 0 to 50
for Galileo channels.
2. Assigning an SV channel will set the Channel Assignment bit to 1 for forced assignment in the Channel
3. The doppler field applies to L1 GPS and Galileo channels only.
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Chapter 5
Commands
Syntax:
Message ID: 27
ASSIGN CHANNEL [ STATE ] [ PRN [ DOPPLER WINDOW ] ]
Field
Name
Binary Binary
Field
Valid Values
Description
Format
Bytes
Offset
1
header
H
0
SV channel number to apply the command
to. 0 is the first SV channel and 15 is the last:
16GPSL1L5:
0-7 for GPSL1 and
8-15 for GPSL5
2
channel 0 to 15
ULong
4
H
10GALILEO6GPS: 0-9 for GALL1 and
10-15 for GPSL1
See also Section 5.3.3, CHANCONFIG
Optional desired SV channel state. If a value
3
4
state
prn
0 to 37 for GPS
Enum
Long
4
4
H+4
H+8
is not given, the default of ACTIVE is used.
Optional satellite PRN code. A value is
120 to 138 for GEO required only when the state field is set to
0 to 50 for GAL
ACTIVE.
Optional current L1 Doppler offset of the
satellite specified in the prn field in Hz.
NOTE:Satellite motion, receiver antenna
motion, and receiver clock frequency error
must be included in the calculation of
Doppler frequency.
5
6
doppler -100 000 to 100 000
window 0 to 10 000
Long
4
4
H+12
H+16
Error or uncertainty in the L1 Doppler
estimate given in the doppler field, in Hz.
NOTE:This is a ± value. For example, enter
500 for ± 500 Hz.
ULong
Examples:
ASSIGN 0 ACTIVE 37 0 2000
ASSIGN 15 120 -250 0
ASSIGN 11 28 -250 0
The first example sets the first SV channel to acquire satellite PRN 37 in a range from -2000 Hz to +2000 Hz
until the satellite signal has been detected. SV channel 11 is set to acquire satellite PRN 28 at an offset of
-250 Hz only in the third example.
Table 18: Channel State Values
ASCII
IDLE
Description
Set the SV channel to not track any satellites.
Set the SV channel active.
ACTIVE
AUTO
Tell the receiver to automatically assign PRN codes to channels.
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Chapter 5
5.3.3
CHANCONFIG
This command changes the channel configuration of the receiver. This will effect the number of channels
tracking GPS signals and the number of channels tracking GEO signals. Entering this command will reset the
receiver, causing the receiver to initiate a cold-start bootup and reset all data stored in NVM to factory default
values (except for the channel configuration).
The default configuration of the L1L5GPS(T) model is 16GPSL1L5 while for the L1E5AGAL(T) model it is
10GALILEO6GPS. If you have a L1E5AGAL(T) model you will also be able to track Galileo and GPS
satellites. If you have an L1L5GPS(T) model you will be able to track GPS but not Galileo satellites.
Syntax:
Message ID: 501
CHANCONFIG CONFIG
Field
Field
Binary Binary
Valid Values
Description
Format
Name
Bytes
Offset
This field contains the Abbreviated ASCII command name. See
1
2
header
config
H
0
Specifies the channel
configuration for the receiver Enum
to use.
4
H
Example:
CHANCONFIG 16GPSL1L5
Table 19: Configuration Values
Description
ASCII
16GPSL1L5
8 GPS L1 + 8 GPS L5 channels
5 Galileo L1 + 5 Galileo E5a + 6 GPS L1 channels
10GALILEO6GPS
a
5 Galileo Data L1 + 5 Galileo Data E5a + 6 GPS L1 channels
8 Galileo L1 + 8 Galileo E5a channels
10GALILEODATA6GPS
16GALILEOL1E5a
8GPS8GEO
8 GPS L1 + 4 GEO L1 + 4 GEO L5 channels
6 GPS L1 + 6 GPS L5 + 2 GEO L1 + 2 GEO L5 channels
16 GPS L5 channels
12GPS4GEOL1L5
16GPSL5
a. Use the 10GALILEODATA6GPS configuration when tracking the GIOVE-A
satellite. GIOVE-A uses a different signal structure than the Galileo SIS-ICD,
therefore the receiver tracks the data signal.
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Chapter 5
Commands
5.3.4
CLOCKADJUST
All oscillators have some inherent drift. By default the receiver attempts to steer the receiver’s clock to
accurately match GPS time. If for some reason this is not desired, this behavior can be disabled using the
ꢀ 1. The CLOCKADJUST command should only be used by advanced users.
2. If the CLOCKADJUST command is ENABLED, and the receiver is configured to use an external
- TCXO, OCXO, RUBIDIUM, CESIUM, or USER), then the clock steering process will take over
the VARF output pins.
3. When disabled, the range measurement bias errors will continue to accumulate with clock drift.
4. Pseudorange, carrier phase and Doppler measurements may jump if the CLOCKADJUST mode is
altered while the receiver is tracking.
5. When disabled, the time reported on all logs may be offset from GPS time. The 1PPS output may
Abbreviated ASCII Syntax:
CLOCKADJUST SWITCH
Message ID: 15
Field
Type
ASCII
Value
Binary
Value
Binary Binary Binary
Field
Description
Format
Bytes
Offset
1
header
H
0
This field contains the Abbreviated ASCII command name.
2
switch
DISABLE
ENABLE
0
1
Disallow adjustment of
internal clock.
Enum
4
H
Allow adjustment of
internal clock.
ASCII Example:
CLOCKADJUST DISABLE
50
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Commands
Chapter 5
5.3.5
COM Serial Port Configuration Control
This command permits you to configure the receiver’s asynchronous serial port communications drivers.
Syntax:
Message ID: 4
COM [PORT ]BPS[ PARITY [DATABITS [ STOPBITS [HANDSHAKE [ECHO [BREAK]]]]]]
Field
Name
Binary Binary
Bytes Offset
Field
Valid Values
Description
Format
1
header
H
0
Serial port to apply the settings to.
2
port
Enum
4
H
settings are applied to COM1.
9600, 19200, 38400,
57600, 115200, or
3
4
H+4
H+8
bps
Communication baud rate (bps)
ULong
Enum
4
4
a
230400
Parity. If not specified, no parity
parity
is assumed.
5
6
7
8
9
databits
stopbits
7 or 8
1 or 2
Number of data bits
Number of stop bits
ULong
ULong
Enum
Enum
Enum
4
4
4
4
4
H+12
H+16
H+20
H+24
H+28
echo
break
a. Baud rates higher than 115,200 bps are not supported by standard PC hardware. Special PC
hardware is required for higher rates, such as 230,400 bps.
Example:
COM COM3 57600 N 8 1 N OFF ON
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Chapter 5
Commands
Table 20: Parity Values
ASCII
Description
N
E
No parity
Even parity
Odd parity
O
Table 21: Handshaking Values
ASCII Description
N
No handshaking
XON
CTS
XON/XOFF software handshaking
CTS/RTS hardware handshaking
Table 22: Echo Values
Description
ASCII
OFF
ON
No echo
Transmit any input characters as they
are received.
Table 23: Break Values
ASCII
Description
Disable break detection
Enable break detection
OFF
ON
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Commands
Chapter 5
5.3.6
ECUTOFF Set Satellite Elevation Cut-off
This command sets the elevation cut-off angle for tracked satellites. The receiver will not track a satellite until
it rises above the cut-off angle. Tracked satellites that fall below the cut-off angle will no longer be tracked
unless they were manually assigned using the ASSIGN command.
In either case, satellites below the ECUTOFF angle will be eliminated from the internal position and clock
offset solution computations.
If the receiver has not yet received an almanac, satellites below the cut-off angle may be tracked.
This command permits a negative cut-off angle, which could be used in these situations:
•
•
the antenna is at a high altitude, and thus can look below the local horizon
satellites are visible below the horizon due to atmospheric refraction
ꢀ 1. This command only affects GPS satellites. GEO and Galileo satellites maintain their lock.
2. Care must be taken when using ECUTOFF because the signals from lower elevation satellites are
travelling through more atmosphere and are therefore degraded.
Syntax:
Message ID: 50
ECUTOFF ANGLE
Field
Field
Binary Binary
Bytes Offset
Valid Values
Description
Format
Name
This field contains the Abbreviated ASCII command name. See
1
2
header
angle
H
0
Elevation cut-off angle
relative to horizon in
degrees.
Float
4
H
-90.0 to +90.0
Example:
ECUTOFF 10.0
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Chapter 5
Commands
5.3.7
EXTERNALCLOCK
Overview
The EXTERNALCLOCK command allows the EuroPak-15a to operate with an optional external oscillator.
You are able to optimally adjust the clock model parameters of the receiver for various types of external clocks.
2. If the EXTERNALCLOCK command is enabled and set for an external clock (TCXO, OCXO,
ENABLED, then the clock steering process will take over the VARF output pins. If clocksteering
is not used with the external oscillator, the clocksteering process must be disabled by using the
CLOCKADJUST DISABLE command.
There are three steps involved in using an external oscillator:
1.
2.
3.
connect an external oscillator to your EuroPak-15a enclosure.
Using the EXTERNALCLOCK command, select a standard oscillator and its operating
frequency.
Using the CLOCKADJUST command, disable the clocksteering process if external
clocksteering is not used.
Theory
An unsteered oscillator can be approximated by a three-state clock model, with two states representing the
range bias and range bias rate, and a third state assumed to be a Gauss-Markov (GM) process representing the
range bias error generated from satellite clock dither. The third state is included because the Kalman filter
assumes an (unmodeled) white input error. The significant correlated errors produced by satellite clock dither
are obviously not white and the Markov process is an attempt to handle this kind of short-term variation.
The internal units of the new clock model’s three states (offset, drift and GM state) are meters, meters per
second, and meters. When scaled to time units for the output log, these become seconds, seconds per second,
and seconds, respectively. Note that the old units of the third clock state (drift rate) were meters per second per
second.
The user has control over 3 process noise elements of the linear portion of the clock model. Namely, the h , h ,
0
-1
and h elements of the power law spectral density model used to describe the frequency noise characteristics of
-2
oscillators:
h–2 h–1
2
Sy(f) = ------- + ------- + h0 + h1 f + h2 f
f 2
f
where f is the sampling frequency and S (f) is the clock’s power spectrum. Typically only h , h , and h affect
y
0
-1
-2
the clock’s Allan variance and the clock model’s process noise elements.
Usage
Before using an optional external oscillator, several clock model parameters must be set. There are default
settings for a voltage-controlled temperature-compensated crystal oscillator (VCTCXO), ovenized crystal
oscillator (OCXO), Rubidium and Cesium standard, which are given in Table 25 on Page 55. Or, the user may
choose to supply customized settings.
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Chapter 5
Abbreviated ASCII Syntax:
EXTERNALCLOCK CLOCKTYPE [FREQ ][h0 [ h1 [ h2 ]]]
Message ID: 230
Field
Type
ASCII Binary
Value Value
Binary Binary Binary
Field
Description
Format
Bytes
Offset
1
header
H
0
This field contains the Abbreviated ASCII command name. See
2
3
clocktype
freq
See Table 24 on
Clock type
Enum
4
4
H
0MHz
5MHz
10MHz
20MHz
0
1
2
3
Optional frequency. If a value is not Enum
specified, the default is 5 MHz.
H+4
4
5
6
h0
h1
h2
1.0 e-31 to 1.0 e-18 Optional timing standards. These
fields are only valid when the USER
Double
Double
Double
8
8
8
H+8
H+16
H+24
1.0 e-31 to 1.0 e-18
clocktype is selected.
1.0 e-31 to 1.0 e-18
ASCII Example:
EXTERNALCLOCK DISABLE
or
EXTERNALCLOCK USER 10MHZ 1.0167E-23 6.87621E-25 8.1762E-26
or
EXTERNALCLOCK TCXO 5MHZ
Table 24: Clock Type
ASCII
DISABLE
TCXO
Binary
Description
0
1
2
3
4
5
Turns the external clock input off, reverts back to the on-board VCTCXO
Sets the pre-defined values for a VCTCXO
OCXO
Sets the pre-defined values for an OCXO
RUBIDIUM
CESIUM
USER
Sets the pre-defined values for a rubidium oscillator
Sets the pre-defined values for a cesium oscillator
Defines custom process noise elements
Table 25: Pre-Defined Values for Oscillators
h
h
h
Clock Type
VCTCXO
0
-1
-2
1.0 e-21
1.0 e-20
1.0 e-20
OCXO
2.51 e-26
1.0 e-23
2.0 e-20
2.51 e-23
1.0 e-22
7.0 e-23
2.51 e-22
1.3 e-26
4.0 e-29
Rubidium
Cesium
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Chapter 5
Commands
5.3.8
FIX Constrain to Fixed Position
This command fixes position parameters for the EuroPak-15a. For various applications, fixing this value can
assist in improving acquisition times and accuracy of position or corrections.
Syntax:
Message ID: 44
FIX TYPE [ LAT LONG HEIGHT ]
Field
Name
Binary Binary
Field
Valid Values
Description
Format
Bytes
Offset
1
2
header
H
0
type
lat
Fix type
Enum
4
8
H
Latitude parameter for a fixed
position in degrees. Only entered
when the fix type is set to
POSITION.
3
4
5
-90 to +90
Double
H+4
Longitude parameter for a fixed
position in degrees. Only entered
when the fix type is set to
POSITION.
long
-360 to +360
Double
Double
8
8
H+12
H+20
Ellipsoidal height parameter for a
fixed position in metres.Only
entered when the fix type is set to
POSITION.
height
-1000 to +20000000
Example:
FIX POSITION 51.116381983333 -114.03829231944 1048.215
Table 26: Fix Type Values
ASCII
NONE
POSITION
Description
Unfix or none. Clears any previous FIX commands.
Configures the receiver with its position fixed.
The receiver performs all computations based on WGS84, which is
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Commands
Chapter 5
- Definitions -
*
Origin = Earth's center of mass
Parallel to the direction of the Conventional Terrestrial Pole (CTP) for
polar motion, as defined by the Bureau International de l'Heure (BIH) on
the basis of the coordinates adopted for the BIH stations.
Z-Axis =
Intersection of the WGS 84 Reference Meridian Plane and the plane of
the CTP's Equator, the Reference Meridian being parallel to the Zero
Meridian defined by the BIH on the basis of the coordinates adopted for
the BIH stations.
X-Axis =
Completes a right-handed, earth-centered, earth-fixed (ECEF)
orthogonal coordinate system, measured in the plane of the CTP
Equator, 90 East of the X-Axis.
Y -Axis =
BIH - Defined CTP
(1984.0)
Z
WGS 84
ω
Earth's Center
of Mass
BIH-Defined
Zero Meridian
(1984.0)
Y
WGS 84
X
WGS 84
*
Analogous to the BIH Defined Conventional Terrestrial System (CTS), or BTS,
1984.0.
Figure 4: The WGS84 ECEF Coordinate System
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Chapter 5
Commands
5.3.9
FRESET Clear Data in NVM
This command clears data which is stored in the receiver’s non-volatile memory and restores the receiver to
factory default settings. The receiver is forced to hardware reset.
Syntax:
Message ID: 20
FRESET
Field
Name
Binary Binary
Field
Valid Values
Description
Format
Bytes
Offset
1
2
header
H
0
Reserved field required for Binary format only. Set to 0 when entering the
Enum
4
H
command in Binary.
Example:
FRESET
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Chapter 5
5.3.10 LOG Request Logs from Receiver
Many different types of data can be logged using several different methods of triggering the log events. See
Chapter 6, Data Logs starting on Page 70 for further information and a complete list of data log structures.
The hold parameter, which is only valid when the ONTIME trigger is being used, will prevent a log from being
removed when the UNLOGALL command is issued. To remove a log which was invoked using the hold
parameter requires the specific use of the UNLOG command.
The period and offset parameters are only valid when the ONTIME trigger is being used as well. For example,
to log data at 1 second after every minute you would set the period to 60 and the offset to 1.
ꢀ Maximum flexibility for logging data is provided to you by these logs. You are cautioned, however, to
recognize that each log requested requires additional CPU time and memory buffer space. Too many logs
may result in lost data and degraded CPU performance. Receiver overload can be monitored using the
Buffer Over-run bits of the Receiver Status word in any log header.
Syntax:
Message ID: 1
LOG [ PORT ] MESSAGE [ TRIGGER ] [ PERIOD [ OFFSET ] [ HOLD ] ]
Valid Values
Field
Name
Binary Binary
Bytes Offset
Field
Description
Format
ASCII
Binary
1
2
header
port
H
0
Serial port at which to
output the log data.
Enum
4
2
H
Any valid message
name, with a suffix to
Any valid
message ID
3
H+4
message specify the output format
as explained in Section
Log to output
UShort
message This field is only present in Binary format.
4
5
Message type of log.
Char
Char
1
1
H+6
H+7
Reserved field required for Binary format only. Set to 0 when entering the
command in Binary.
Trigger, or condition,
to generate log on.
6
trigger
Enum
4
H+8
Log period for
ONTIME trigger in
seconds
7
8
period
offset
Any positive double value.
Double
Double
8
8
H+12
H+20
Any positive double value smaller than
the value specified in the period field.
Offset for ONTIME
trigger in seconds.
Flag for whether or
not the log is removed
by the UNLOGALL
command. Valid for
ONTIME trigger only.
9
hold
Enum
4
H+28
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Chapter 5
Examples:
Commands
LOG COM1 PSRPOSA ONTIME 7 2.5 HOLD
LOG COM3 PRSPOSA ONCE
The first example configures the EuroPak-15a to output the PSRPOS log in ASCII format to COM1 at 7 second
intervals offset by 2.5 seconds (output at 2.5 seconds then 9.5 seconds and so on). The second example outputs
the log only once on COM3.
Table 27: Log Trigger Values
ASCII
ONNEW
Binary
Description
Output when the message is updated (not
necessarily changed).
0
ONCHANGED
ONTIME
ONNEXT
ONCE
1
2
3
4
Output when the message is changed.
Output on a time interval.
Output only the next message.
Output only the current message.
Table 28: Log Hold Values
ASCII
Binary
Description
Allow log to be removed by the
UNLOGALL command.
NOHOLD
0
Prevent log from being removed by the
UNLOGALL command.
HOLD
1
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Chapter 5
5.3.11 POSITIONTYPE Set the Position Solution
This command sets the position filter to compute the position on either the GPS L1 or GPS L5 frequencies. You
can also obtain data from a specific frequency. Both position and navigation data are available on GPS L1 or
GPS L5. The ephemeris and almanac are decoded on the selected frequency.
When using simulated signals, if the L1 and L5 constellations are different, the receiver may drop signals that
are not in view based on the almanac. For example, if the receiver is tracking PRN 15 on L5, the position type
is set to GPSL1 and the L1 almanac indicates that PRN 15 is not in view, then the receiver stops tracking PRN
15.
To prevent this:
•
•
•
Change the position type frequency with the POSITIONTYPE command, or
Ensure the constellations in the simulations agree with what you expect to track
ꢀ This command only affects GPS satellites. Galileo satellites maintain their lock.
Syntax:
Message ID: 836
POSITIONTYPE FREQUENCY
Field
Binary Binary
Field
Valid Values
Description
Format
Name
header
frequency
Bytes
Offset
1
2
H
0
GPSL1 or GPSL5
4
H
Example:
POSITIONTYPE GPSL1
Table 29: Position Frequency Switch
ASCII
Description
GPSL1
GPSL5
GPS L1 frequency
GPS L5 frequency
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Chapter 5
Commands
5.3.12 PULSEBLANKING Enable/Disable Pulse Blanking
ꢀ The PULSEBLANKING command should only be used by advanced users.
This command enables or disables digital pulse blanking. By default, the digital pulse blanking is enabled. The
sensitivity of the digital pulse blanking may be adjusted using the switch field.
Syntax:
PULSEBLANKING
Message ID: 519
FREQUENCY
SWITCH
Field
Name
Binary
Bytes
Binary
Offset
Field
Valid Values
Description
Format
This field contains the Abbreviated ASCII command name. See
1
header
H
0
Pulse blanking frequency. See
Table 30 below.
Enum
Ulong
2
3
frequency
switch
4
4
H
L1 or L5
0-127
Pulse blanking switch using
H+4
Examples:
PULSEBLANKING L1 5
Table 30: Frequency Switch
Description
ASCII
L1
GPS L1 and Galileo L1 frequency
GPS L5 and Galileo E5a frequency
L5
Table 31: Pulse Blanking Switch
ASCII
0
Description
Disable pulse blanking
Enable pulse blanking
1-127
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Chapter 5
5.3.13 RESET Hardware Reset
This command performs a hardware reset. Following a RESET command, the receiver will initiate a cold-start
bootup and will retain the most recent receiver configuration (that is, channel configuration).
The optional delay field is used to set the number of seconds the receiver is to wait before resetting.
Syntax:
Message ID: 18
RESET [ DELAY ]
Field
Field
Binary Binary
Valid Values
Description
Format
Name
Bytes
Offset
1
2
header
delay
H
0
Seconds to wait before resetting. If no
Any ulong value.
value is provided, the default of 0
seconds is assumed.
ULong
4
H
Example:
RESET 5
See also the FRESET command.
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Chapter 5
Commands
5.3.14 SDLLBW Configure DLL Filter Bandwidth
This is the noise equivalent bandwidth command for the signal channel DLL filter bandwidth.
ꢀ 1. The SDLLBW command should only be used by advanced users. It may not be suitable for every
application. When using SDLLBW in a differential mode, the same setting should be used at both the
monitor and remote station.
2. When you issue the SDLLBW command, all channels lose lock and the locktime for all tracking
satellites is reset to zero.
3. The measurement becomes noisier as the DLL bandwidth increases.
Syntax:
Message ID: 800
SDLLBW DSIGCHAN
BW
Field
Field
Binary Binary
Bytes Offset
Valid Values
Description
Format
Name
This field contains the Abbreviated ASCII command name. See
1
2
3
header
dsigchan
bw
H
0
The parameters should be applied
0-15
Ulong
Float
4
4
H
to this signal channel.
Noise equivalent bandwidth of
DLL filter in Hz.
H+4
0.001-0.5
Example:
SDLLBW 0 0.01
64
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Chapter 5
5.3.15 SPLLBW Configure Phase-Lock-Loop Bandwidth
ꢀ 1. This command can fundamentally change the way that the receiver operates. Do not alter the default
settings unless you are confident that you understand the consequences.
2. When you change this command, the selected channel loses lock and the locktime for its tracking
satellite is reset to zero.
3. The log order for the C/A signal is 3rd order.
This command sets the PLL low-pass filter bandwidth for one signal channel.
A time filtered square of the L1 carrier phase tracking loop error signal is used to track the performance of this
tracking loop. This value is used as the variance of L1 carrier phase measurements. The threshold specified by
this command is compared with the loop variance to determine when the signal tracking lock time is reset. The
resetting of the signal lock time is used to indicate that conditions exist in which a cycle slip might occur.
The time filtering that is performed on the loop variance determination is controlled using the third argument of
this command. This value is used to compute the first order time constant that provides a noise equivalent
bandwidth for the specified bandwidth. The filtering equation used is:
-ΔTω
-ΔTω
new value = e
× (old data) + (1 - e
) × (new data)
where
ΔT = the PLL sampling rate, and
ω = 4 × filter constant
Syntax:
Message ID: 801
SPLLBW PSIGCHAN BW
Field
Name
Binary Binary
Bytes Offset
Field
Valid Values
Description
Format
1
header
H
0
The parameters should be applied to
2
3
psigchan
bw
0-15
Ulong
4
4
H
this signal channel.
PLL low-pass filter bandwidth in Hz. Float
H+4
Example:
SPLLBW 0 1.0
Table 32: PLL Bandwidth Values
Frequency
Valid Bandwidth Values
GPS C/A signals
Galileo L1 signals
Galileo E5a signals
0.5 to 15 Hz
0.5 to 15 Hz
0.5 to 15 Hz
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Chapter 5
Commands
5.3.16 STHRESHOLD Control Signal Thresholds
This command controls signal acquisition and steady-state-lock signal thresholds. The sigchan, acqui, lock and
crosscorr fields must have values. They set the thresholds for the specified L1 channel.
ꢀ When you change this command, the selected channel loses lock and the locktime for its tracking satellite
is reset to zero.
Syntax:
Message ID: 803
STHRESHOLD SIGCHAN ACQUI LOCK CROSSCORR
Field
Name
Binary Binary
Field
Valid Values
Description
Format
Bytes
Offset
1
2
header
H
0
The parameters should be applied
sigchan
0-15
Ulong
4
H+20
to this signal channel.
Acquisition power threshold in
dBHz.
3
4
acqui
lock
25-80
10-80
ULong
ULong
4
4
H
Steady-state tracking lock
threshold in dBHz.
H+4
Specifies the cross-correlation
power threshold in dBHz, at which ULong
point, the checks are performed.
5
crosscorr
4
H+8
10-80
Example:
STHRESHOLD 0 35 20 35
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Commands
Chapter 5
5.3.17 UNASSIGN Unassign a Previously Assigned Channel
This command cancels a previously issued ASSIGN command and the SV channel reverts to automatic control.
Syntax:
Message ID: 29
UNASSIGN CHANNEL
Field
Field
Binary Binary
Valid Values
Description
Format
Name
Bytes
Offset
1
header
H
0
Previously selected SV channel
to apply automatic search and
2
3
channel 0 to 15
ULong
Enum
4
4
H
acquisition mode, see also
Reserved field required for Binary format only. Set to 2 when entering the
H+4
command in Binary.
Example:
UNASSIGN 11
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Chapter 5
Commands
5.3.18 UNLOG Remove Log from Logging Control
This command permits you to remove a specific log request from the system.
Syntax:
Message ID: 36
UNLOG [ PORT ] DATATYPE
Valid Values
Field
Binary Binary
Field
Description
Format
Name
Bytes
Offset
ASCII
Binary
1
header
H
0
Serial port at which log is
being output. If a value is
2
3
port
Enum
4
4
H
not provided, COM1 is
assumed.
datatype Message name
Message ID
Log to be disabled.
ULong
H+4
Example:
UNLOG COM3 PSRPOSA
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Commands
Chapter 5
5.3.19 UNLOGALL Remove All Logs from Logging Control
This command disables all logs on the specified port only. All other ports are unaffected.
ꢀ This command does not disable logs that have the HOLD attribute set. (See the LOG command in Section
5.3.10 on Page 59 for more information on this attribute). To disable logs with the HOLD attribute, use the
UNLOG command.
Syntax:
Message ID: 38
UNLOGALL [ PORT ]
Field
Name
Binary Binary
Field
Valid Values
Description
Format
Bytes
Offset
1
header
H
0
Serial port at which logging is to
2
3
port
disabled. If a value is not provided,
Enum
Enum
4
4
H
COM1 is assumed.
Reserved (always 0).
H+4
Example:
UNLOGALL
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Chapter 6
Data Logs
6.1 Functional Listing of Logs
Table 33 lists the logs by function and provides the type of each log. The valid types are discussed in Section
Table 33: Logs By Function
Log
Description
Type
GENERAL RECEIVER CONTROL AND STATUS
AGCSTATS
Automatic gain control status
Synch
Polled
Synch
Synch
Polled
RXCOMMANDS
RXSECSTATUS
SYSTEMLEVELS
VERSION
Receiver configuration information
Receiver section status
System hardware levels
Receiver hardware and software version numbers
POSITION, PARAMETERS, AND SOLUTION FILTERING CONTROL
PSRPOS
Position data
Synch
CLOCK INFORMATION, STATUS, AND TIME
Range bias information
CLOCKMODEL
TIME
Synch
Synch
Receiver time information
POST PROCESSING DATA
Satellite range information
RANGE
Synch
SATELLITE TRACKING AND CHANNEL CONTROL
Current decoded almanac data
Satellite range information
ALMANAC
RANGE
Asynch
Synch
RAWEPHEM
RAWFRAME
SATVIS
Raw ephemeris
Asynch
Asynch
Synch
Raw subframes
Satellite azimuth and elevation angle data
Channel tracking information
TRACKSTAT
Synch
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Chapter 6
6.2 Log Summary
Table 34: Log Summary
Message ID
Log Name
Description
AGCSTATS
ALMANAC
630
73
Automatic gain control status
Current decoded almanac data
Current clock model matrices
Position data
CLOCKMODEL
PSRPOS
16
47
RANGE
43
Satellite range information
Raw ephemeris
RAWEPHEM
RAWFRAME
RXCOMMANDS
RXSECSTATUS
SATVIS
41
804
579
638
48
Raw subframes
Receiver configuration information
Receiver section status
Satellite azimuth and elevation angle data
System hardware levels
SYSTEMLEVELS
TIME
653
101
83
Receiver time information
Channel tracking information
Receiver hardware and software version numbers
TRACKSTAT
VERSION
37
6.3 Log Reference
For each log, the recommended input command for generating the log is provided. The recommended
command is shown in ASCII format, unless otherwise specified. An example of the log output, in ASCII format,
is provided for each recommended input.
ꢀ All logs are followed by a carriage return and line feed. However, in some of the examples, carriage
returns have been inserted in the middle of the log to clearly indicate different data sets.
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Chapter 6
Data Logs
6.3.1
AGCSTATS Automatic Gain Control Status
This log provides status information for the automatic gain control mechanism and details of the parameters it
is currently using.
Log Type: Synch
Message ID: 630
Field
Field
Binary
Bytes
Binary
Offset
Data Description
Format
Name
This field contains the message header, in ASCII or Binary format.
1
header
H
0
2
# RF decks Number of RF decks reported in this message.
Ulong
4
4
4
4
4
8
8
8
8
8
8
8
8
8
H
3
AGCword
gain
Ulong
H+4
4
AGC gain (0 to 99999)
Ulong
H+8
5
pulse width VARF pulse width
Ulong
H+12
H+16
H+20
H+28
H+36
H+44
H+52
H+60
H+68
H+76
H+84
6
modulus
bin1
VARF modulus
Ulong
7
A/D bin 1 (decimal percentage)
A/D bin 2 (decimal percentage)
A/D bin 3 (decimal percentage)
A/D bin 4 (decimal percentage)
A/D bin 5 (decimal percentage)
A/D bin 6 (decimal percentage)
Double
Double
Double
Double
Double
Double
Double
Double
Double
8
bin2
9
bin3
10
11
12
13
14
15
16...
bin4
bin5
bin6
noise floor Calculated noise floor
Reserved
Next RF deck, offset = H+ 4 + (#RF *88) Bytes
32-bit CRC (ASCII and Binary only)
H+ 4
(#RF*88)
Hex
4
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Chapter 6
Table 35: AGC Status Word
Description Bit = 0
Bit
Bit = 1
0
Jam Detected
Jamming Not Present
Jamming Present
1
AGC Calibrated
Coarse Calibration = 0
Fine Calibration = 1
2
3
RF Type
1 = L1
2 = L2
3 = L5/E5a
4
5
6
ADC Range indicates which 3 bits of the 0 = Bits 7, 6, 5
8-bit ADC output are currently being
used by the receiver.
1 = Bits 7, 5, 4
2 = Bits 7, 4, 3
3 = Bits 7, 3, 2
4 = Bits 7, 2, 1
5 = Bits 7, 1, 0
7
8
9
Method of Noise Floor Calculation
1 = AGC
2 = Post Correlation
3 = …
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
Reserved
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Chapter 6
Data Logs
Recommended Input:
LOG AGCSTATSA ONTIME 10
Example Output:
#AGCSTATSA,COM1,0,78.0,FINE,338,320316.822,00A00000,0000,33331;
2,
28A,8493,3893,8000,0.0383,0.1064,0.2175,0.2853,0.2162,0.1364,
1283057.375000,-0.009275,0.000000,
29A,8037,3437,8000,0.0905,0.1543,0.2492,0.2490,0.1627,0.0944,
1273863.750000,-0.008741,0.000000*A05AE5E7
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Data Logs
Chapter 6
6.3.2
ALMANAC Decoded Almanac
This log contains the decoded almanac parameters for the frequency specified in the POSITIONTYPE
command, see Page 61. Multiple messages are transmitted, one for each SV almanac collected. For more
information on Almanac data, refer to the GPS SPS Signal Specification. A list of standards and references
with contact information can be found in the GPS+ Reference Manual available on our website at http://
www.novatel.com/support/docupdates.htm.
Log Type: Asynch
Message ID: 73
Field
Field
Binary
Bytes
Binary
Offset
Description
Format
Name
This field contains the message header, in ASCII or Binary format.
1
header
H
0
2
3
4
5
6
#msg
PRN
The number of satellite PRN almanac data sets to follow. Long
Satellite PRN number for current message, dimensionless ULong
4
4
4
8
8
H
H+4
H+8
H+12
H+20
week
seconds
ecc
Almanac reference week (GPS week number)
Almanac reference time, seconds into the week
Eccentricity, dimensionless
ULong
Double
Double
°
7
8
Rate of right ascension, radians/second
Right ascension, radians
Double
Double
8
8
H+28
H+36
ω
ω0
ω
9
Argument of perigee, radians
Double
Double
Double
8
8
8
H+44
H+52
H+60
o
10
11
M
Mean anomaly of reference time, radians
Clock aging parameter, seconds
a
fo
a
12
13
14
15
16
17
18
19
20...
Clock aging parameter, seconds/second
Corrected mean motion, radians/second
Semi-major axis, meters
Double
Double
Double
Double
ULong
ULong
ULong
Enum
8
8
8
8
4
4
4
4
H+68
f1
N
H+76
A
H+84
incl-angle
SV config
health-prn
health-alm
antispoof
Angle of inclination relative to 0.3 π, radians
Satellite configuration
H+92
H+100
H+104
H+108
H+112
SV health from subframe 4 or 5
SV health from almanac
Next almanac data set, offset = H + 4 + (# previous msg x 112)
H + 4 +
(112 x
#msg)
21
32-bit CRC (ASCII and Binary only)
Hex
4
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Chapter 6
Data Logs
Recommended Input:
LOG ALMANACA ONCHANGED
ASCII Example:
#ALMANACA,COM1,0,78.0,SATTIME,338,320004.000,00A00000,0000,33331;
29,
1,338,503808.0,6.318092E-03,-7.60031658E-09,-1.96827599E+00,
-1.70715209E+00,-1.27284116E+00,3.71932983E-05,3.63797881E-12,
1.45856914E-04,2.65599916E+07,4.42098057E-02,1,0,0,TRUE,
2,338,503808.0,9.141445E-03,-8.26320134E-09,2.18251798E+00,
1.97852363E+00,1.88691247E-01,-1.81198120E-05,0.00000000E+000,
1.45860977E-04,2.65594983E+07,8.63463404E-03,1,0,0,FALSE,
3,338,503808.0,7.876873E-03,-8.11462372E-09,1.04690369E+00,
6.62592815E-01,-6.81532759E-01,7.53402710E-05,3.63797881E-12,
1.45858780E-04,2.65597651E+07,-1.61187825E-02,1,0,0,TRUE,
4,338,503808.0,7.454395E-03,-8.27463039E-09,2.20228558E+00,
1.45160422E-01,2.49410670E+00,1.52587891E-04,1.09139364E-11,
1.45848996E-04,2.65609528E+07,8.20919406E-03,1,0,0,FALSE,
...
27,338,503808.0,1.979542E-02,-8.16033991E-09,-1.01833966E+00,
-1.95538209E+00,2.34013039E+00,3.62396240E-05,0.00000000E+000,
1.45857411E-04,2.65599312E+07,1.44709516E-02,1,0,0,FALSE,
28,338,503808.0,1.103687E-02,-7.84032658E-09,1.06756599E-01,
-2.28547146E+00,1.17978552E+00,3.33786011E-05,0.00000000E+000,
1.45859194E-04,2.65597148E+07,1.80602269E-02,1,0,0,TRUE,
29,338,503808.0,9.426594E-03,-7.60031658E-09,-2.01631026E+00,
-9.70531593E-01,7.15315540E-01,5.36918640E-04,1.09139364E-11,
1.45855712E-04,2.65601375E+07,4.33289651E-02,1,0,0,TRUE,
30,338,503808.0,8.715153E-03,-8.02319134E-09,5.43083877E-02,
1.29254172E+00,1.52598431E+00,2.57492065E-05,3.63797881E-12,
1.45865786E-04,2.65589145E+07,2.19311316E-03,1,0,0,FALSE
*2E0D3E7A
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Data Logs
Chapter 6
6.3.3
CLOCKMODEL Current Clock Model Status
The CLOCKMODEL log contains the current clock-model status of the receiver.
Monitoring the CLOCKMODEL log will allow you to determine the error in your receiver reference oscillator
as compared to the GPS satellite reference.
All logs report GPS time not corrected for local receiver clock error. To derive the closest GPS time, subtract
the clock offset from the GPS time reported. The clock offset can be calculated by dividing the value of the
range bias given in field 6 of the CLOCKMODEL log by the speed of light (c).
The following symbols are used throughout this section:
B =
Range bias (m)
BR = Range bias rate (m/s)
SAB = Gauss-Markov process representing range bias error due to SA clock dither (m)
The standard clock model now used is as follows:
clock parameters array = [ B BR SAB]
covariance matrix =
2
σ
σ
σ
σ
σ
B
B
BR
B
SAB
2
σ
σ
σ
σ
σ
BR
B
BR
BR SAB
2
σ
σ
σ
σ
σ
SAB
B
SAB BR
SAB
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Chapter 6
Log Type: Synch
Data Logs
Message ID: 16
Binary
Bytes
Binary
Offset
Field
Field Name
header
Description
Format
This field contains the message header, in ASCII or Binary format.
1
H
0
Clock model status as computed from current
Enum
2
clock status
4
H
3
reject
Number of rejected range bias measurements
GPS time of last noise addition
GPS time of last update
ULong
GPSec
GPSec
4
4
4
8
8
8
8
8
8
8
8
8
8
8
8
H+4
4
noise time
update time
H+8
5
H+12
H+16
H+24
H+32
H+40
H+48
H+56
H+64
H+72
H+80
H+88
H+96
H+104
6
Clock correction parameters (a 1x3 array of length 3),
listed left-to-right
7
parameters
Double
8
9
10
11
12
13
14
15
16
17
Covariance of the straight line fit (a 3x3 array of length
9), listed left-to-right by rows
cov data
Double
Last instantaneous measurement of the range bias
(meters)
18
19
range bias
range bias rate
change
Double
Double
8
8
H+112
H+120
Last instantaneous measurement of the range bias rate
(m/s)
Indicates whether or not there is a change in the
20
21
Enum
Hex
4
4
H+128
H+132
32-bit CRC (ASCII and Binary only)
78
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Chapter 6
Recommended Input:
LOG CLOCKMODELA ONTIME 1
Example Output:
#CLOCKMODELA,COM1,0,55.0,FINE,1048,497224.500,
00000128,879E,0;VALID,0,497224.500,497224.500,6.59596736E-01,-
9.29232987E-02,-3.40165918E+00,4.63006778E+02,1.19966616E+00,-
4.50054493E+02,1.19966616E+00,2.15673338E-01,-7.90256149E-01,-
4.50054493E+02,-7.90256149E-01,4.76057122E+02,-2.902,-1.03659974E-
01,FALSE*f33b4465
Table 36: Clock Model Status Values
ASCII
VALID
Binary
Description
The clock model is valid
0
1
2
3
4
CONVERGING
ITERATING
INVALID
The clock model is near validity
The clock model is iterating towards validity
The clock model is not valid
Clock model error
ERROR
Table 37: Constellation Change Flag Values
ASCII
FALSE
Binary
Description
0
1
There has not been a change in the constellation
The constellation has changed
TRUE
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Chapter 6
Data Logs
6.3.4
PSRPOS Pseudorange Position
This log contains the pseudorange position computed by the receiver, along with three status flags.
Log Type: Synch
Message ID: 47
Field
Name
Binary Binary
Field
Description
Format
Bytes
Offset
This field contains the message header, in ASCII or Binary format.
1
header
H
0
2
3
4
5
6
7
sol status
pos type
lat
Enum
Enum
Double
Double
Double
Float
4
4
8
8
8
4
H
Latitude (percentage degrees)
H+4
H+8
H+16
H+24
H+32
lon
Longitude (percentage degrees)
Height above ellipsoid (m)
hgt
Reserved
datum id#
Datum ID number. This will always be 61 for the WGS84
coordinate system.
8
9
Enum
4
H+36
lat σ
Float
Float
4
4
H+40
H+44
Latitude standard deviation (m)
10
lon σ
Longitude standard deviation (m)
Height standard deviation (m)
11
12
13
14
hgt σ
Float
4
4
4
4
H+48
H+52
H+56
H+60
Char[4]
Float
Reserved
Float
Number of observations tracked for signal type being
used in position solution.
15
#obs
UChar
1
H+64
16
17
18
19
20
21
22
#obs in pos Number of observations used in position
UChar
UChar
UChar
UChar
UChar
UChar
UChar
1
1
1
1
1
1
1
H+65
H+66
H+67
H+68
H+69
H+70
H+71
Reserved
23
32-bit CRC (ASCII and Binary only)
Hex
4
H+72
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Chapter 6
Recommended Input:
LOG PSRPOSA ONTIME 1
Example Output:
#PSRPOSA,COM1,0,58.0,FINE,1027,324231.000,00000000,FC91,0;
SOL_COMPUTED,SINGLE,51.11615533807,-114.03850611829,1010.452,-
16.271,61,19.50677306162,14.52973740177,39.584,”0”,0.0,60.000,9,8,
8,1,0,0,0,0*de152df7
Table 38: Solution Status Values
ASCII
Binary
Description
SOL_COMPUTED
INSUFFICIENT_OBS
NO_CONVERGENCE
SINGULARITY
0
1
2
3
4
Solution computed
Insufficient observations
No convergence
Singularity at parameters matrix
Covariance trace exceeds maximum (trace > 1000 m)
CONV_TRACE
Test distance exceeded (maximum of 3 rejections if
distance > 10 km)
TEST_DIST
COLD_START
V_H_LIMIT
5
6
7
Not yet converged from cold start
Height or velocity limits exceeded (in accordance with
COCOM export licensing restrictions)
VARIANCE
8
9
Variance exceeds limits
Residuals are too large
Delta position is too large
Negative variance
RESIDUALS
DELTA_POS
NEGATIVE_VAR
10
11
Table 39: Position Type Values
ASCII
Binary
Description
NONE
0
No solution
Position has been fixed by the FIX POSITION command
FIXEDPOS
SINGLE
1
or by position averaging
16
Single point position
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Chapter 6
Data Logs
6.3.5
RANGE Satellite Range Information
RANGE contains the channel measurements for the currently tracked satellites. When using this log, please
keep in mind the constraints noted along with the description.
It is important to ensure that the receiver clock model is valid. This can be monitored by the bits in the Receiver
Status field of the log header. Large jumps in pseudorange as well as accumulated Doppler range (ADR) will
occur as the clock is being adjusted. If the ADR measurement is being used in precise phase processing, it is
important not to use the ADR if the parity known flag in the ch-tr-status field is not set as there may exist a half
(1/2) cycle ambiguity on the measurement. The tracking error estimate of the pseudorange and carrier phase
(ADR) is the thermal noise of the receiver tracking loops only. It does not account for possible multipath errors
or atmospheric delays.
If a PRN is being tracked on more than one signal (GPS L1, GPS L5, Galileo L1 or Galileo E5a) multiple
entries with the same PRN will appear in the range logs. As shown in Table 40 on Page 84, these entries can be
differentiated by bits 21-22 of the ch-tr-status field, which denote whether the observation is for GPS L1, GPS
L5, Galileo L1 or Galileo E5a. This is to aid in parsing data.
Log Type: Synch
Message ID: 43
Field
Name
Binary
Bytes
Binary
Offset
Field
Description
Format
This field contains the message header, in ASCII or Binary format. See
1
2
header
H
0
# obs
Number of data sets to follow.
Long
4
H
3
4
5
6
7
8
9
PRN
Satellite PRN number of range measurement.
UShort
UShort
Double
Float
2
2
8
4
8
4
4
H+4
Reserved
psr
H+6
Pseudorange measurement (m).
H+8
psr std
adr
Pseudorange measurement standard deviation (m).
Carrier phase, in cycles (accumulated Doppler range).
Estimated carrier phase standard deviation (cycles).
Instantaneous carrier Doppler frequency (Hz).
Carrier to noise density ratio
H+16
H+20
H+28
H+32
Double
Float
adr std
dopp
Float
C/N
0
10
11
Float
4
4
4
H+36
H+40
H+44
C/N = 10[log (S/N )] (dB-Hz)
0
10
0
Number of seconds of continuous tracking (no cycle
slipping).
locktime
Float
ch-tr-
status
12
ULong
13...
Next data set, offset = H + 4 + (# previous obs x 44)
H+4+
(#obs x
44)
variable 32-bit CRC (ASCII and Binary only)
Hex
4
82
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Data Logs
Chapter 6
Recommended Input:
LOG RANGEA ONTIME 30
Example Output:
#RANGEA,COM1,0,86.0,FREEWHEELING,336,158190.000,00E80000,0000,33331
;6,
7,0,23349304.589,0.280,-122701400.419,0.008,-2905.889,43.4,
7344.640,08005C04,
2,0,20669493.328,0.159,-108618920.523,0.005,-1639.363,48.4,
7343.750,08005C24,
25,0,24880354.627,0.376,-130747143.832,0.009,370.102,40.9,
1179.550,08005C44,
5,0,21128558.586,0.141,-111031319.590,0.004,-2245.102,49.4,
7340.550,08005C64,
6,0,22572830.405,0.307,-118621049.557,0.008,2665.866,42.7,
3916.040,08005C84,
30,0,20727099.269,0.179,-108921652.406,0.004,-196.892,47.3,
6596.850,08005CA4*FAE4A508
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Chapter 6
Nibble #
N0
Data Logs
Table 40: Channel Tracking Status
Description
Bit #
Mask
Range Value
0
0x00000001
0x00000002
0x00000004
0x00000008
0x00000010
0x00000020
0x00000040
0x00000080
0x00000100
0x00000200
0x00000400
0x00000800
0x00001000
0x00002000
0x00004000
0x00008000
0x00010000
0x00020000
0x00040000
1
0 to 22
2
Tracking state
3
4
5
N1
N2
N3
N4
6
0-n (0 = first, n = last)
n depends on the receiver
7
SV channel number
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
Phase lock flag
Parity known flag
Code locked flag
0 = Not locked, 1 = Locked
0 = Not known, 1 = Known
0 = Not locked, 1 = Locked
Correlator spacing
Satellite system
0 = GPS
1, 4-7 = Reserved
2 = GEO
3 = Galileo
Reserved (always 0)
Reserved (always 0)
0x00200000
N5
N6
If GPS/GEO:
0 = L1 C/A
If Galileo:
0x00400000
0 = L1 dataless
5 = L2 P
1 = L1 data
Signal Type
(depends on satellite system)
0x00800000
0x01000000
0x02000000
0x04000000
9 = L2 P codeless
14 = L5 C5 dataless
26 = L5 C5 data
10 = E5a dataless
11 = E5a data
15 = E5b dataless
30 = L5 C5 combined 16 = E5b data
Forward Error Correction (FEC)
0 = Not FEC, 1 = FEC
Reserved (always 0)
Continued on Page 85
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Data Logs
Chapter 6
Nibble #
Bit #
28
Mask
Description
Range Value
0x10000000
0x20000000
Reserved for future use
29
30
31
N7
Reserved (always 0)
0x80000000 Channel assignment
0 = Automatic, 1 = Forced
Table 41: Tracking State Bit Values
Bit Value
Description
0
1
Idle
Sky search
2
Wide frequency band pull-in
Narrow frequency band pull-in
PLL
3
4
5
Reacquisition
6
Steering
7
Frequency-lock loop
Reserved
8-14
15
Neumann-Hoffman alignment
Table 42: Correlator Spacing Bit Values
Bit Value
Description
0
1
2
3
4
Reserved
Standard correlator: spacing > 0.1 chip
Narrow correlator: spacing = 0.1 chip
Reserved
Reserved
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Chapter 6
Data Logs
6.3.6
RAWEPHEM Raw Ephemeris
This log contains the raw binary information for subframes one, two and three from a satellite with the parity
information removed. Each subframe is 240 bits long (10 words - 24 bits each) and the log contains a total 720
bits (90 bytes) of information (240 bits x 3 subframes). This information is preceded by the PRN number of the
satellite from which it originated. This message is not generated unless all 10 words from all 3 frames have
passed parity.
Ephemeris data whose Time Of Ephemeris (TOE) is older than six hours is not shown.
Log Type: Asynch
Message ID: 41
Binary Binary
Bytes Offset
Field Field Name
Description
Format
This field contains the message header, in ASCII or Binary
1
header
H
0
2
3
4
5
6
7
8
prn
Satellite PRN number
Ephemeris reference week number
Ephemeris reference time (seconds.)
Subframe 1 data.
Ulong
Ulong
Ulong
Hex
4
H
ref week
ref secs
4
H+4
4
H+8
subframe1
subframe2
subframe3
30
30
32
4
H+12
H+42
H+72
H+104
Subframe 2 data.
Hex
Subframe 3 data.
Hex
32-bit CRC (ASCII and Binary only)
Hex
Recommended Input:
LOG RAWEPHEMA ONCHANGED
Example Output:
#RAWEPHEMA,COM1,7,76.5,SATTIME,338,338430.000,00A00000,0000,33331;
29,338,345600,8B05486E2B255490003CD3E8731DDB8A24F57C45F225546000006
946137A0000000000,8B05486E2BA8250A4E2BB771090CD2097204D3A7FB1250A10
D95B354607D000000B2EA,8B05486E2C2F0072ADE5E6AE005C2829DA2F1B93D8620
667FFAAFC250D9A0000000000*D413845E
...
#RAWEPHEMA,COM1,4,76.5,SATTIME,338,338430.000,00A00000,0000,33331;
10,338,345584,8B05486E2B255490003CD3E8731DDB8A24F57C45FB94545F00000
50A52E70000000000,8B05486E2BA894FC2A2D01670FCEA8FCC0039DF4691822A10
C7F8E545F2B000000B2EA,8B05486E2C2FFFBA8488C0FDFFD127BDA71614E90FD78
438FFABE494F11E0000000000*6854985A
...
#RAWEPHEMA,COM1,0,76.5,SATTIME,338,338430.000,00A00000,0000,33331;
15,338,345600,8B05486E2B255492012CD3E8731DDB8A24F57C45FB56546000003
44A40460000000000,8B05486E2BA856FD4936E4E87361D4FD2F04D0F1270900A10
DA76554607C000000B2EA,8B05486E2C2FFFFD5C183A3FFFBE27061AC724B767F70
A30FFA2F056FDD40000000000*71B1AC43
86
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Data Logs
Chapter 6
6.3.7
RAWFRAME Raw Subframes
This log contains the raw subframes. The subframes are output even when there are parity failures.
Log Type: Asynch Message ID: 804
Binary Binary
Bytes Offset
Field
Field Name
Description
Format
This field contains the message header, in ASCII or Binary
1
2
header
H
0
The parameters should be applied to this
signal channel.
sigchan
PRN
ULong
4
H
3
4
5
6
7
Satellite PRN number
ULong
4
4
4
4
H+4
#parity failures Number of words that had parity failures
Ulong
H+12
H+8
#bits in frame
#bytes
Number of bits in subframe
Number of bytes to follow
Raw subframe data
ULong
Ulong
H+16
H+20
a
data
Hex[variable]
40
8
32-bit CRC (ASCII and Binary only)
Hex
4
H+60
a. In the Binary log case, the data field will only output the number of bits in the subframe. This is 120 for L1
and 244 for E5a.
Recommended Input:
LOG RAWFRAMEA ONNEW
Example Output:
#RAWFRAMEA,COM1,0,82.5,SATTIME,343,408162.000,004C0000,0000,33331;
0,25,0,300,38,
8B055C85EC8749C007DBB52D155C1600602633471F30DDE8937A78CB99790057570
AFFFAF140*AEC280E1
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Chapter 6
Data Logs
6.3.8
RXCOMMANDS Receiver Configuration
This log outputs all of the current receiver configuration parameters set using the commands in Chapter 5.
When requested, one RXCOMMANDS log is output for each command type. The embedded message is the
most-recent command string entered by you for that command type. If you have not yet entered a command
string for that command type, the default configuration values from start-up are provided.
Log Type: Polled
Message ID: 579
Field Field Name
Data Description
Format
Bytes
Offset
This field contains the message header, in ASCII or Binary format.
1
2
header
H
4
0
command
type
Indicates which command the embedded message
Int
H
Embedded message of the most-recent command
string you entered. If a command string has not been
entered yet, the default values from start-up will be
provided.
Uchar
[variable]
3
4
e msg
variable
4
H+4
32-bit CRC (ASCII and Binary only)
Hex
variable
Recommended Input:
LOG RXCOMMANDSA ONCE
Example Output:
#RXCOMMANDSA,COM1,59,77.5,FINE,334,237306.911,00E40008,0000,33331;
4,COM COM1 9600 N 8 1 N OFF ON*A5267A8D
#RXCOMMANDSA,COM1,58,77.5,FINE,334,237306.914,00E40008,0000,33331;
20,CHANCONFIG 16GPSL1L5*63C63093
#RXCOMMANDSA,COM1,57,77.5,FINE,334,237306.914,00E40008,0000,33331;
5,ECUTOFF 10.0*B85DB8B9
#RXCOMMANDSA,COM1,56,77.5,FINE,334,237306.916,00E40008,0000,33331;
7,FIX NONE*BC3BA5EC
#RXCOMMANDSA,COM1,55,77.5,FINE,334,237306.916,00E40008,0000,33331;
21,PULSEBLANKING L1 127*EC7B5565
#RXCOMMANDSA,COM1,54,77.5,FINE,334,237306.916,00E40008,0000,33331;
21,PULSEBLANKING L5 127*409DCBCE
#RXCOMMANDSA,COM1,53,77.5,FINE,334,237306.919,00E40008,0000,33331;
39,DLLORDER GPS 1*63D03A14
#RXCOMMANDSA,COM1,52,77.5,FINE,334,237306.919,00E40008,0000,33331;
2,ANTENNAPOWER OFF*100A691D
#RXCOMMANDSA,COM1,51,77.5,FINE,334,237306.919,00E40008,0000,33331;
3,CLOCKADJUST DISABLE*CBDEACCB
#RXCOMMANDSA,COM1,50,77.5,FINE,334,237306.921,00E40008,0000,33331;
4,COM COM3 115200 N 8 1 N OFF ON*9FA0AF3C
#RXCOMMANDSA,COM1,49,77.5,FINE,334,237306.921,00E40008,0000,33331;
47,POSITIONTYPE GPSL1*F455BBD0
#RXCOMMANDSA,COM1,32,77.5,FINE,334,237306.937,00E40008,0000,33331;
45,SDLLBW 0 0.2000*287F8BC9
#RXCOMMANDSA,COM1,31,77.5,FINE,334,237306.939,00E40008,0000,33331;
45,SDLLBW 1 0.2000*91909AD3
88
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Data Logs
Chapter 6
#RXCOMMANDSA,COM1,30,77.5,FINE,334,237306.939,00E40008,0000,33331;
45,SDLLBW 2 0.2000*9FF5CFD6
#RXCOMMANDSA,COM1,29,77.5,FINE,334,237306.942,00E40008,0000,33331;
45,SDLLBW 3 0.2000*E3127AD4
#RXCOMMANDSA,COM1,28,77.5,FINE,334,237306.942,00E40008,0000,33331;
45,SDLLBW 4 0.2000*693D212B
#RXCOMMANDSA,COM1,27,77.5,FINE,334,237306.944,00E40008,0000,33331;
45,SDLLBW 5 0.2000*18EF7223
#RXCOMMANDSA,COM1,26,77.5,FINE,334,237306.944,00E40008,0000,33331;
45,SDLLBW 6 0.2000*168A2726
#RXCOMMANDSA,COM1,25,77.5,FINE,334,237306.944,00E40008,0000,33331;
45,SDLLBW 7 0.2000*806FD6D3
#RXCOMMANDSA,COM1,24,77.5,FINE,334,237306.946,00E40008,0000,33331;
45,SDLLBW 8 0.2000*5C5DB456
#RXCOMMANDSA,COM1,23,77.5,FINE,334,237306.947,00E40008,0000,33331;
45,SDLLBW 9 0.2000*0BC696BF
#RXCOMMANDSA,COM1,22,77.5,FINE,334,237306.947,00E40008,0000,33331;
45,SDLLBW 10 0.2000*A29D2B26
#RXCOMMANDSA,COM1,21,77.5,FINE,334,237306.950,00E40008,0000,33331;
45,SDLLBW 11 0.2000*E0C1A1D3
#RXCOMMANDSA,COM1,20,77.5,FINE,334,237306.950,00E40008,0000,33331;
45,SDLLBW 12 0.2000*27A70B2F
#RXCOMMANDSA,COM1,19,77.5,FINE,334,237306.952,00E40008,0000,33331;
45,SDLLBW 13 0.2000*C7D7C93F
#RXCOMMANDSA,COM1,18,77.5,FINE,334,237306.952,00E40008,0000,33331;
45,SDLLBW 14 0.2000*84FB6D39
#RXCOMMANDSA,COM1,17,77.5,FINE,334,237306.954,00E40008,0000,33331;
45,SDLLBW 15 0.2000*51802385
#RXCOMMANDSA,COM1,16,77.5,FINE,334,237306.954,00E40008,0000,33331;
46,SPLLBW 0 3.0000*E2D11BF7
#RXCOMMANDSA,COM1,15,77.5,FINE,334,237306.957,00E40008,0000,33331;
46,SPLLBW 1 3.0000*5E885A8A
#RXCOMMANDSA,COM1,14,77.5,FINE,334,237306.957,00E40008,0000,33331;
46,SPLLBW 2 3.0000*50ED0F8F
#RXCOMMANDSA,COM1,13,77.5,FINE,334,237306.959,00E40008,0000,33331;
46,SPLLBW 3 3.0000*87385FCE
#RXCOMMANDSA,COM1,12,77.5,FINE,334,237306.959,00E40008,0000,33331;
46,SPLLBW 4 3.0000*0D170431
#RXCOMMANDSA,COM1,11,77.5,FINE,334,237306.961,00E40008,0000,33331;
46,SPLLBW 5 3.0000*02C8C399
#RXCOMMANDSA,COM1,10,77.5,FINE,334,237306.961,00E40008,0000,33331;
46,SPLLBW 6 3.0000*0CAD969C
#RXCOMMANDSA,COM1,9,77.5,FINE,334,237306.963,00E40008,0000,33331;
46,SPLLBW 7 3.0000*2E2CDD3F
#RXCOMMANDSA,COM1,8,77.5,FINE,334,237306.963,00E40008,0000,33331;
46,SPLLBW 8 3.0000*77E69D75
#RXCOMMANDSA,COM1,7,77.5,FINE,334,237306.963,00E40008,0000,33331;
46,SPLLBW 9 3.0000*534DAF6D
#RXCOMMANDSA,COM1,6,77.5,FINE,334,237306.964,00E40008,0000,33331;
46,SPLLBW 10 3.0000*5858199B
#RXCOMMANDSA,COM1,5,77.5,FINE,334,237306.964,00E40008,0000,33331;
46,SPLLBW 11 3.0000*4EC8EE24
#RXCOMMANDSA,COM1,4,77.5,FINE,334,237306.964,00E40008,0000,33331;
46,SPLLBW 12 3.0000*89AE44D8
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Chapter 6
Data Logs
#RXCOMMANDSA,COM1,3,77.5,FINE,334,237306.966,00E40008,0000,33331;
46,SPLLBW 13 3.0000*68B72659
#RXCOMMANDSA,COM1,2,77.5,FINE,334,237306.966,00E40008,0000,33331;
46,SPLLBW 14 3.0000*2B9B825F
#RXCOMMANDSA,COM1,1,77.5,FINE,334,237306.966,00E40008,0000,33331;
46,SPLLBW 15 3.0000*3D0B75E0
#RXCOMMANDSA,COM1,0,77.5,FINE,334,237306.969,00E40008,0000,33331;
6,EXTERNALCLOCK OCXO 10MHZ 0.000000 0.000000 0.000000*CB079FDA
Table 43: Command Type Values
ASCII
BINARY
Command
0
1-2
3
0
1-2
3
ASSIGN
Reserved
CLOCKADJUST
COM
4
4
5
5
ECUTOFF
EXTERNALCLOCK
FIX
6
6
7
7
8
8
FRESET
9
9
LOG
10
11-18
19
20
21
22
23-24
25
26
27-42
43
44
45
46
47
10
11-18
19
20
21
22
23-24
25
26
27-42
43
44
45
46
47
RESET
Reserved
AGCMODE
CHANCONFIG
PULSEBLANKING
UNLOG
Reserved
UNLOGALL
UNASSIGN
Reserved
STHRESHOLD
Reserved
SDLLBW
SPLLBW
POSITIONTYPE
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Data Logs
Chapter 6
6.3.9
RXSECSTATUS Receiver Section Status
This log is used to output the version and status information for each receiver card in the receiver section.
Log Type: Synchronous
Message ID: 638
Field
Field
Binary Binary
Bytes Offset
Description
Format
Name
This field contains the message header, in ASCII or Binary format.
1
header
H
0
2
3
4
5
6
7
8
# comp
type
Number of components (cards, and so on)
Ulong
Enum
Enum
4
4
4
H
H+4
H+8
H+12
H+28
H+44
H+60
Reserved
model
Model
Char[16] 16
Char[16] 16
Char[16] 16
psn
Product serial number
Firmware software version
sw version
Ulong
Ulong
Ulong
4
4
4
Receiver error word. A value of zero indicates no
error word
9
H+64
H+68
10
Reserved
11...
Next component offset = H + 4 + (#comp x 68)
H+4+
(#comp
x 68)
variable
32-bit CRC (ASCII and Binary only)
Hex
4
Recommended Input:
LOG RXSECSTATUSA ONNEW
Example Output:
#RXSECSTATUSA,COM1,0,78.0,FINE,338,320380.000,00A00000,0000,33331;
1,L1E5A,PM,"L1E5AGALT","DZN05140006","5.000D24",00A00000,00000000,
00401000*3FD5F86C
Table 44: Component Type
ASCII
Binary
Description
Unknown component
UNKNOWN
GPSCARD
FPGA
0
1
5
Receiver component
Field Programmable Gate Array
CLKSTAT
L5EURO
CPLD
6
7
8
9
Reserved
Reserved
Complex programmable logic device
Reserved
L1E5A
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Chapter 6
Data Logs
Table 45: Receiver Error
Nibble # Bit #
Mask
Description
Dynamic Random Access Memory (DRAM) status
Reserved
Bit = 0
OK
Bit = 1
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
Error
N0
N1
N2
N3
N4
0
0x00000001
0x00000002
0x00000004
0x00000008
0x00000010
0x00000020
0x00000040
0x00000080
0x00000100
0x00000200
0x00000400
0x00000800
0x00001000
0x00002000
0x00004000
0x00008000
0x00010000
0x00020000
0x00040000
0x00080000
1
OK
2
OK
3
OK
4
Electronic Serial Number (ESN) access status
Authorization code status
Reserved
OK
5
OK
6
OK
7
Supply voltage status
Reserved
OK
8
OK
9
Temperature status (as compared against acceptable limits) OK
10
11
12
13
14
15
16
17
18
19
MINOS4 status (FPGA)
PLL RF1 hardware status - L1
PLL RF2 hardware status - L5
Reserved
OK
OK
OK
OK
OK
OK
OK
OK
OK
OK
NVM status
Stack usage status
Memory usage status
Message queue usage status
Message usage status
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Data Logs
Chapter 6
Table 46: Receiver Status
Description
Nibble # Bit #
Mask
Bit = 0
No error
Bit = 1
Error
0
N0
1
2
3
4
5
6
7
8
9
0x00000002 Temperature status
0x00000004 Voltage supply status
0x00000008 Antenna power status
0x00000010 LNA status
Within specifications Warning
OK
Warning
Not powered
Failure
Powered
OK
0x00000020 Antenna open flag
0x00000040 Antenna shorted flag
0x00000080 CPU overload flag
0x00000100 COM1 buffer overrun flag
0x00000200 Reserved
OK
Open
N1
N2
OK
Shorted
Overload
Overrun
No overload
No overrun
10
11
12
13
0x00000400 COM3 buffer overrun flag
No overrun
Overrun
0x00000800
0x00001000
0x00002000
Reserved
N3
N4
14
15
16
17
18
19
20
21
22
23
0x00004000
0x00008000
0x00010000
0x00020000
0x00040000 Almanac flag
Valid
Valid
Invalid
0x00080000 Position solution flag
Invalid
Fixed
0x00200000 Clock steering status
0x00400000 Clock model flag
0x00800000 External oscillator flag
Enabled
Disabled
Invalid
N5
Valid
PLL not locked
PLL locked
24
25
26
27
0x01000000 Stack warning
OK
OK
OK
OK
Warning
Warning
Warning
Warning
0x02000000
0x04000000
0x08000000
Memory warning
N6
N7
Message queue warning
Message block usage warning
Reserved
28
29
0x10000000
0x20000000
30
31
0x40000000
0x80000000 AUX1 status event flag
No event
Event
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Chapter 6
Data Logs
6.3.10 SATVIS Satellite Visibility
This log outputs satellite visibility data and additional satellite information based on the specified position type.
Log Type: Synch
Message ID: 48
Field
Name
Binary
Bytes
Binary
Offset
Field
Description
Format
This field contains the message header, in ASCII or Binary
1
2
header
H
0
Indicates if the satellite visibility is valid. See
sat vis
Enum
4
H
Indicates if the complete almanac was used. See
3
4
5
comp alm
#sat
Enum
ULong
Short
4
4
2
H+4
H+8
H+12
Number of satellite data sets to follow
GPS satellite PRN number of range measurement
(GPS only).
PRN
6
7
8
9
Reserved
health
elev
Short
2
4
8
8
8
8
H+14
H+16
H+20
H+28
H+36
H+44
a
ULong
Double
Double
Double
Double
Satellite health
Elevation (degrees)
az
Azimuth (degrees)
10
11
12
true dop
app dop
Theoretical Doppler of satellite (Hz)
Apparent Doppler for this receiver (Hz)
Next satellite data set, offset = H + 12 + (# previous sat x 40)
H+12+
(#sat x 40)
variable 32-bit CRC (ASCII and Binary only)
Hex
4
a. Satellite health values may be found in ICD-GPS-200. To obtain copies of ICD-GPS-200, refer to ARINC. A
list of standards and references with contact information can be found in the GPS+ Reference Manual
Recommended Input:
LOG SATVISA ONTIME 60
ASCII Example:
#SATVISA,COM1,0,44.0,FINE,1039,490308.000,00000028,6002,0;
TRUE,TRUE,27,
14,0,0,74.5,267.4,458.2,458.926672761,
25,0,0,61.3,73.7,-1252.6,-1251.902056196,
1,0,0,55.9,277.4,1799.2,1799.897879028,
16,0,0,33.6,305.9,2874.8,2875.534296744,
...
26,0,0,-82.0,114.8,-188.9,-188.237459086*bf8c9522
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Data Logs
Chapter 6
Table 47: Satellite Visibility Values
ASCII
FALSE
TRUE
Binary
Description
0
1
Satellite visibility is invalid
Satellite visibility is valid
Table 48: Complete Almanac Flag Values
ASCII
Binary
Description
FALSE
TRUE
0
1
Complete almanac was not used
Complete almanac was used
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Chapter 6
Data Logs
6.3.11 SYSTEMLEVELS System Hardware Levels
This log contains environmental and voltage parameters for the receiver card.
Log Type: Synchronous
Message ID: 653
Binary
Bytes
Binary
Offset
Field
Field Name
Data Description
Format
This field contains the message header, in ASCII or Binary
1
header
H
0
2
3
4
5
6
7
8
9
# comp
type
Number of components
Ulong
Enum
Enum
Float
Float
Float
Float
Float
Float
Float
Float
Float
Float
4
4
4
4
4
4
4
4
4
4
4
4
4
H
H + 4
H + 8
H + 12
H + 16
H + 20
H + 24
H+28
H+32
H+36
H+40
H+44
H+48
Reserved
temp
Board temperature (°C)
ant current
core volt
supply volt
RF volt
Approximate internal antenna current (A)
1V CPU core voltage (V)
12V supply voltage (V)
5V RF supply voltage (V)
Internal LNA voltage (V)
3.3 V supply voltage
10
LNA volt
3.3 V supply
11
12
TCXO control volt Control voltage for TCXO
13
idle time
Idle time (%)
14
LNA output volt
LNA output voltage (V)
15…
Next component offset = H + 4 + (# comp x 48)
H + 4 + (#
comp x 48)
variable 32-bit CRC (ASCII and Binary only)
Hex
4
Recommended Input:
LOG SYSTEMLEVELSA ONTIME 1
Example Output:
#SYSTEMLEVELSA,COM1,0,77.5,FINE,338,320405.000,00A00000,0000,33331;
1,
L1E5A,PM,58.000,0.138,1.194,11.636,4.985,4.564,3.230,1.588,77.880,
4.223*B5E852BE
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Data Logs
Chapter 6
6.3.12 TIME Time Data
This log is output at the Time port at a maximum rate of 1 Hz and provides the GPS time of the receiver’s 1 PPS
signal. It also includes the information on the receiver clock offset and the clock model status.
Log Type: Sync
Message ID: 101
Field
Name
Binary Binary
Field
Description
Format
Bytes
Offset
This field contains the message header, in ASCII or Binary format. See
1
header
H
0
Clock model status (not including current measurement
Enum
2
3
clock status
offset
4
8
H
Receiver clock offset, in seconds from GPS time. A positive
offset implies that the receiver clock is ahead of GPS time.
Double
H+4
To derive GPS time, use the following formula:
GPS time = receiver time - offset
4
offset std
Reserved
Receiver clock offset standard deviation (s)
Double
Hex
8
H+12
H+20
H+44
5-12
13
24
4
32-bit CRC (ASCII and Binary only)
Recommended Input:
LOG TIMEA ONTIME 1
Example Output:
#TIMEA,COM1,0,58.0,FINE,1049,248050.000,00000128,5C46,0;
VALID,-0.000000002,0.000001901,-13.00000000294,2000,2,15,20,53,
57011,VALID*d6f14d5d
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Chapter 6
Data Logs
6.3.13 TRACKSTAT Tracking Status
These logs provide channel tracking status information for each of the receiver’s channels.
Log Type: Synch
Message ID: 83
Field
Name
Binary
Bytes
Binary
Offset
Field
Description
Format
This field contains the message header, in ASCII or Binary
1
header
H
0
2
3
4
5
6
7
8
9
sol status
pos type
cutoff
Primary antenna low elevation cut-off angle
Number of hardware channel data sets to follow
Satellite PRN number of range measurement
Enum
Enum
Float
Long
Short
Short
4
4
4
4
2
2
4
8
4
4
H
H+4
H+8
# chans
PRN
H+12
H+16
H+18
H+20
H+24
H+32
H+38
Reserved
psr
Pseudorange (m)
Double
Float
10
11
Doppler
C/No
Doppler frequency (Hz)
Carrier to noise density ratio (dB-Hz)
Float
Number of seconds of continuous tracking (no
cycle slips)
12
13
14
locktime
psr res
Float
4
4
4
4
H+42
H+46
H+50
H+54
Pseudorange residual from pseudorange filter (m) Float
Range reject code from pseudorange filter. See
reject
Enum
15
psr weight
Pseudorange filter weighting
Float
16...
Next hardware channel data set, offset = H+16 + (# previous chans x 40)
32-bit CRC (ASCII and Binary only) Hex
H+16 +
(#chans x 40)
variable
4
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Data Logs
Chapter 6
Recommended Input:
LOG TRACKSTATA ONTIME 1
Example Output:
#TRACKSTATA,COM1,0,64.5,FINE,1048,507426.700,00000028,228E,0;
SOL_COMPUTED,SINGLE,0.0,24,
5,0,8105C04,25052294.167,3388.063,40.188,63.560,7.209,GOOD, 1.000,
...
2,0,1305C2B,21433408.821,1310.921,43.913,514.040,0.000,OBSL2, 1.000,
...
26,0,1305D6B,24444419.776,2365.217,31.530,1506.520,0.000,OBSL2,
1.000
*cd40e0aa
Table 49: Reject Code Values
ASCII
Binary
Description
GOOD
0
1
2
3
4
5
6
Observations are good
BADHEALTH
Bad satellite health is indicated by ephemeris data
OLDEPHEMERIS
Old ephemeris due to date not being updated during the last 3 hours
Eccentric anomaly error during computation of the satellite’s position
True anomaly error during computation of the satellite’s position
Satellite coordinate error during computation of the satellite’s position
Elevation error due to the satellite being below the cut-off angle
ECCENTRICANOMALY
TRUEANOMALY
SATCOORDINATEERROR
ELEVATIONERROR
Misclosure too large due to excessive gap between estimated and actual
positions
MISCLOSURE
NOEPHEMERIS
INVALIDIODE
7
9
Ephemeris data for this satellite has not yet been received
Invalid IODE (Issue Of Data Ephemeris) due to mismatch between
differential stations
10
Low power meaning that the satellite is rejected due to low carrier/noise
ratio
LOWPOWER
12
16
17
No compatible ionospheric correction is available for this particular
satellite
NOIONOCORR
BAD_INTEGRITY
Bad integrity indicating a large variation between the measured range to
the satellite and the theoretical range computed from the ephemeris
OBSL5
GALL1
GALE5a
OBSL1
NA
18
19
20
23
99
Tracking a GPS or SBAS L5 signal that is not used in a position solution
Tracking a Galileo L1 signal
Tracking a Galileo E5a signal
Tracking a GPS or SBAS L1 signal that is not used in a position solution
No observation (a reject code is not applicable)
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Chapter 6
Data Logs
6.3.14 VERSION Version Information
This log contains the version information for all components of a system. When using a standard receiver, there
will only be one component in the log.
Log Type: Polled
Message ID: 37
Field
Name
Binary Binary
Field
Description
Format
Bytes
Offset
This field contains the message header, in ASCII or Binary format. See
1
2
header
H
0
# comp
Number of components (cards, etc.)
Long
4
4
H
3
4
5
type
model
psn
Model
Enum
H+4
H+8
H+24
Char[16] 16
Char[16] 16
Product serial number
hw
6
7
8
9
Char[16] 16
H+40
H+56
H+72
H+88
H+100
version
sw
version
Char[16]
16
boot
version
Char[16] 16
Char[12] 12
Char[12] 12
comp
date
comp
time
10
11...
Next component, offset = H + 4 + (# previous comp x 108)
H+4+
(#comp
x 108)
variable
32-bit CRC (ASCII and Binary only)
Hex
4
Recommended Input:
LOG VERSIONA ONCE
Example Output:
#VERSIONA,COM1,0,78.0,FINE,338,320423.720,00A00000,0000,33331;
2,
L1E5A,"L1E5AGALT","DZN05140006","L1E5A-1.00-2X2",
"5.000D24","5.000D1DB","2006/FEB/10","11:48:48",
FPGA,"ALTERA","","1.3.52","GALILEO","","2006/JAN/12",
"13:26:48"*C1270A13
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Data Logs
Chapter 6
Table 50: Version Log Field Formats
Field Format
Field Name
Description
P= hardware platform (e.g. OEM4)
R = hardware revision (e.g.3.10)
S = processor revision (e.g. A)
hw version
P-RS-CCC
a
CCC = COM port configuration (e.g. 22T)
VV = major revision number
RRR = minor revision number
X = Special (S), Beta (B),
Internal Development (D, A)
xxx = number
sw version, boot version
VV.RRR[Xxxx]
YYYY = year
MM= month
comp date
comp time
YYYY/MM/DD
HH:MM:SS
DD = day (1 - 31)
HH = hour
MM = minutes
SS = seconds
a. One character for each of the COM ports 1, 2, and 3. Characters are: 2 for RS-232, 4 for RS-422, and
T for LV-TTL. Therefore, the example is for a receiver that uses RS-232 for COM 1 and COM 2 and LV-
TTL for COM 3.
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Chapter 7
Firmware Updates
The receiver firmware is stored in on-board, non-volatile memory, which allows it to be updated in the field.
Therefore, updating firmware takes only a few minutes instead of several days, which would be required if the
receiver had to be sent to a service depot.
When updating to a higher revision level, you will need to transfer the new firmware to the appropriate card
using one of NovAtel’s firmware loading utilities. WinLoader is designed for use with Window-based systems
and was developed for use with Unix-based systems.
Below is shown an outline of the procedure for updating your receiver's firmware:
1. Contact the NovAtel Aviation Group.
2. Download update files.
3. Decompress files.
4. Run the firmware loading utility.
7.1 Contacting the NovAtel Aviation Department
The first step in updating the receiver is to contact the NovAtel Aviation Group via any of the methods
When you call, be sure to have the receiver's serial number and program revision level available. This
Figure 5: Serial Number and Version Label
You can also verify the information by powering up the receiver and requesting the VERSION log.
After conferring with the Aviation Group to establish the required revision level, as well as the terms and
conditions of your firmware update, the Aviation Group will issue you an authorization code or auth-code. The
auth-code is required to unlock the receiver features according to your authorized model type.
If it is determined that you will be updating to a higher revision level with the use of the firmware loading
utility, the Aviation Group will confirm with you as to the procedures, files, and methods required for using this
utility. As the main utility and other necessary files are generally provided in a compressed file format, you will
also be given a file decompression password. The utility and update files are available from the Aviation Group
by FTP, e-mail, or diskette.
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Firmware Updates
Chapter 7
7.2 Downloading the Files
Typically, there are two files required when performing firmware updates on a particular receiver card:
WINLOAD.EXE (the firmware loading utility program)
•
• XXXX.HEX(the firmware update file)
Typical Euro-L1E5a card firmware files might be named 5100.HEX, for example.
To proceed with your update, you will first need to download the appropriate files from NovAtel's FTP site at
ftp.novatel.ca, or via e-mail at [email protected]. If downloading is not possible, the files can be mailed to
you on diskette.
The files are available in compressed, password-protected file format. The compressed form of the files may
have different names than the names discussed above; the Aviation Group will advise you as to the exact names
of the files you need. As well, the Aviation Group will provide you with a file de-compression password.
7.3 Decompressing the Files
After copying the compressed files to an appropriate directory on your computer, each file must be
decompressed. The syntax for decompression is as follows:
Syntax:
[filename][password]
where filename is the name of the compressed file (but not including the .EXE extension) and password is the
password required to allow decompression.
A window-based dialog is provided for password entry.
The self-extracting archive then generates the following files:
WinLoad.exe
HowTo.txt
WinLoad utility program
Instructions on how to use the WinLoad utility
Information on the changes made in the firmware since the last revision
WhatsNew.txt
XXXX.hex
Firmware version update file
where XXXX = program version level (for example 2000.hex)
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Chapter 7
Firmware Updates
7.4 Running the Utility
WinLoad is a windows based program used to download firmware to receiver cards. The main screen is shown
Figure 6: Main Screen of WinLoad
If you are running WinLoad for the first time you will need to make sure the file and communications settings
are correct.
7.4.1
Open a File to Download
Figure 7: WinLoad’s Open Dialog
Once you have selected your file, the name should appear in the main display area and in the title bar, see
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Firmware Updates
Chapter 7
Figure 8: Open File in WinLoad
Table 51: Target Card Identification
Entry
Description
Euro-L1E5a card
0
7.4.2
Communications Settings
To set the communications port and baud rate, select COM Settings from the Settings menu, see Figure 9 on
Page 105. Choose the port on your PC from the Com Port drop down list and the baud rate from the Download
Baudrate drop down list. The baud rate should be as high as possible (the default of 115200 is preferred).
Figure 9: COM Port Setup
7.4.3
Downloading Firmware
To download firmware follow these steps:
4. Click on the Write Flash button to download the firmware:
5. While WinLoad searches for the card, power cycle the receiver (turn it off and then on again).
ꢀ You will only be able to access information from the card and download new firmware during the first few
seconds after power initiation.
6. WinLoad should be able to locate the card and the hex file should start downloading. When the
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Chapter 7
Firmware Updates
Figure 10: Authorization Code Dialog
7. The receiver should finish downloading and reset. The process is complete when “Done.” is
Figure 11: Update Process Complete
8. Close WinLoad.
This completes the procedure required to update a EuroPak-15a receiver.
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Chapter 8
Built-In Status Test
8.1 Overview
The built-in test monitors system performance and status to ensure the receiver is operating within its
specifications. If an exceptional condition is detected, the user is informed through one or more indicators. The
receiver status system is used to configure and monitor these indicators:
1. Receiver status word
2. Error strobe line
3. RXSECSTATUS log
In normal operation the error strobe is driven low. When an unusual and non-fatal event occurs (for example,
there is no valid position solution), a bit is set in the receiver status word. Receiver operation continues
normally and the error strobe remains off. When the event ends (for example, when there is a valid position
solution), the bit in the receiver status word is cleared.
When a fatal event occurs (that is, in the event of a receiver hardware failure), a bit is set in the receiver error
word to indicate the cause of the problem. Bit 0 is set in the receiver status word to show that an error occurred
and the error strobe is driven high. Receiver tracking is disabled at this point but command and log processing
continues to allow you to diagnose the error. Even if the source of the error is corrected at this point, the
receiver must be reset to resume normal operation.
8.2 Receiver Status Word
The receiver status word indicates the current status of the receiver. This word is found in the header of all logs.
8.3 Error Strobe Signal
The error strobe line is one of the I/O strobes and is driven low when the receiver is operating normally. When
the receiver is in the error state and tracking is disabled, the error strobe is driven high. This can be caused by a
fatal error or by an unusual receiver status indication that the user has promoted to be treated like a fatal error.
Once on, the error status will remain high until the cause of the error is corrected and the receiver is reset.
8.4 Receiver Status Log
8.4.1
Overview
The Receiver Status log (RXSECSTATUS) provides information on the current system status and configuration
in a series of hexadecimal words.
The status word is the third last field in the RXSECSTATUS log as shown in Figure 12 on Page 108. It is also
the third last field in the header of every log.
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Chapter 8
Built-In Status Test
<RXSECSTATUSA COM1 0 78.0 FINE 338 320380.000 00a00000 0000 33331
< 1
<
<
L1E5A PM "L1E5AGALT" "DZN05140006"
“5.000D24" 00CC0000 00000000 00401000
Receiver
Status
Word
Figure 12: Location of Receiver Status Word
Each bit in the status word indicates the status of a specific condition or function of the receiver. If the status word is
00000000, the receiver is operating normally. The numbering of the bits is shown in Figure 13 below.
0 0 C C 0 0 0 0
0000 0000 1100 1100 0000 0000 0000 0000
Bit 31
Bit 0
Figure 13: Reading the Bits in the Receiver Status Word
The format of the log is described in Chapter 4 of this manual. If the receiver status word indicates a problem, please
8.4.2
Error Word
The error field contains a 32 bit word. Each bit in the word is used to indicate an error condition. Error conditions may
result in damage to the hardware or erroneous data, so the receiver is put into an error state. If any bit in the error word
is set, the receiver will set the error strobe line, idle all channels, turn off the antenna, and disable the RF hardware.
The only way to get out of the error state is to reset the receiver.
The error word is the second last field in the RXSECSTATUS log, as shown in the example below.
<RXSECSTATUSA COM1 0 78.0 FINE 338 320380.000 00a00000 0000 33331
< 1
<
<
L1E5A PM "L1E5AGALT" "DZN05140006"
“5.000D24" 00A00000 00000000 00401000
Receiver
Error
Word
Figure 14: Location of Receiver Error Word
0 0 0 0 0 0 0 0
0000 0000 0000 0000 0000 0000 0000 0000
Bit 0
Bit 15
Figure 15: Reading the Bits in the Receiver Error Word
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Built-In Status Test
Chapter 8
00000000, the receiver is not experiencing an error condition. If the receiver error word indicates an error,
8.4.3
Status Code Arrays
There are 3 status code arrays – the receiver status word, the auxiliary 1 status and the auxiliary 2 status. The
status word is similar to the error word, with each of its 32 bits indicating a condition.
8.4.4
Receiver Status Code
The receiver status word is included in the header of all logs. It has 32 bits, which indicate certain receiver
conditions. If any of these conditions occur, a bit in the status word is set.
8.4.5
Auxiliary Status Codes
The auxiliary status codes are only seen in the RXSECSTATUS log. The two bits representing the auxiliary
status codes give indication about the receiver state for information only. The bits typically do not cause
degradation of the receiver performance. Bit 31 and bit 32 of the receiver status word corresponds to the
auxiliary 1 and auxiliary 2 status words respectively.
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Appendix A Technical Specifications
Table 52: Performance Specifications
PERFORMANCE
All values subject to GPS system characteristics
Frequency
GPS
Galileo
L1(1575.42 MHz), L5 (1176.45 MHz)
L1 (1575.42 MHz), E5a (1176.45 MHz)
GPS L1-C/A Code
GPS L5 Code
Galileo L1 Code
Codes Tracked
Galileo E5a Code
GPS SVN (PRN 0-37)
GEO SVN (PRN 120-138)
Galileo SVN (PRN 0-50)
Satellite Tracking Channels
Position Accuracy (stand-alone)
1.5 m CEP
Pseudorange Measurement
Accuracy
L1 C/A Narrow
L1 C/A Wide
L5 Code
10 cm RMS, C/No > 44 dB-Hz, DLL BW = 0.05 Hz
1 m RMS, C/No > 44 dB-Hz, DLL BW = 0.05 Hz
1 m RMS, C/No > 44 dB-Hz, DLL BW = 0.05 Hz
1 m RMS, C/No > 44 dB-Hz, DLL BW = 0.05 Hz
L5 GEO Code
Single Channel Phase Accuracy
L1 C/A
L5 Code
3 mm RMS, C/No > 44 dB-Hz, Loop PLL = 3 Hz
3 mm RMS, C/No > 44 dB-Hz, Loop PLL = 3 Hz
C/No Accuracy
C/A
±2.5 dB, 30-65 dB-Hz
±2.5 dB, 30-65 dB-Hz
L5 Code
Raw Data Availability Rate
L1SQM/L5/BOCL1/E5a
Time
One phase and code measurement per second/per satellite
One message per second
Almanac Data
< 15 minutes after reset
100 seconds (95%) with stabilized internal and external oscillators and
initial time, almanac and position.
Time to First Fix
Re-acquisition
L1 C/A
5 seconds C/No = 44 dB-Hz 1σ
60 seconds C/No = 44 dB-Hz 1σ
L5 Code
a
Height Measurements
Up to 18,288 metres (60,000 feet) maximum
a. In accordance with export licensing.
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Technical Specifications
Appendix A
A.1 EuroPak-15a and EuroPak-15aT Enclosures
PHYSICAL
Size
235 x 154 x 71 mm
Weight
1.2 kg maximum (including Euro-L1E5a card)
DIMENSIONS
a b
235
71
a. All dimension are in millimeters, please use the Unit Conversion section of the GPS+
docupdates.html for conversion to imperial measurements.
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Appendix A
Technical Specifications
INPUT/OUTPUT DATA INTERFACE
COM1 AND COM2
RS232
Electrical format
a
9600 (default), 19200, 38400, 57600, 115200, 230400 bps
TX, RX, RTS, CTS, DTR, DCD
Bit rate
Signals supported
a. Baud rates higher than 115,200 bps are not supported by standard PC hardware. Special PC hardware is re-
quired for higher rates, including 230,400 bps.
INPUT/OUTPUT STROBES
MSR (Measure Output)
MKI (Mark Input)
Normally high, active low where the pulse width is 1 ms. The falling edge is the
receiver measurement strobe.
An input mark (negative pulse > 55 ns), time tags output log data to the time of
the falling edge of the mark input pulse.
PV (Position Valid)
ERROR
Output indicates a ‘good solution’ or a valid GPS solution when high.
Output that Indicates fatal error warning when high.
PPS (Pulse Per Second)
Normally high, active low pulse is 1 ms wide @ 1 Hz. Falling edge is used as
the reference.
Reset TTL signal output to external system; active high.
RESETOUT
Output
STROBE ELECTRICAL SPECIFICATIONS
Voltage:
LVTTL levels
Low:
High:
minimum 0 VDC and maximum 0.55 VDC @ 24 mA
minimum 2.4 VDC and maximum 3.6 VDC @ 8 mA
Input
Voltage:
LVTTL levels
Low:
High:
minimum 0 VDC and maximum 0.8 VDC
minimum 2.0 VDC and maximum 5.5 VDC
112
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Technical Specifications
Appendix A
INPUT/OUTPUT CONNECTORS
Antenna Input
TNC female jack, 50 Ω nominal impedance
+5 VDC, 100 mA max
(output from EuroPak-15a to antenna/LNA)
PWR
4-pin LEMO connector
EuroPak-15a
Input Voltage:
+9 to +18 VDC
Power Consumption:
6 W (typical)
EuroPak-15aT
Input Voltage
Power Consumption
+11 to +18 VDC
13 W (typical)
COM1
COM2
AUX
DB9P connector
DB9P connector
DB9P connector (Reserved)
I/O
DB9S connector
a
OSC
BNC connector
Oscillator input on the EuroPak-15a
Input Frequency
Signal Level
5 or 10 MHz ± 0.5 ppm
0 to +13 dBm
Oscillator output on the EuroPak-15aT
Output Frequency
Signal Level
Phase Noise
0.1 Hz
10 MHz
+10 dBm ± 3 dB
-55 dBc/Hz
-95 dBc/Hz
-125 dBc/Hz
-155 dBc/Hz
-165 dBc/Hz
-165 dBc/Hz
-165 dBc/Hz
1 Hz
10 Hz
100 Hz
1 kHz
10 kHz
100 kHz
ENVIRONMENTAL
Operating Temperature
EuroPak-15a:
EuroPak-15aT:
-40°C to +50°C
-20°C to +50°C
Storage Temperature
Humidity
-45°C to +95°C
Not to exceed 95% non-condensing
a. The EuroPak-15a provides an external oscillator input on this connector while the EuroPak-15aT
provides an output from the internal clock.
EuroPak-15a Receiver User Manual Rev 5
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Appendix A
Technical Specifications
A.1.1 Port Pin-Outs
Table 53: EuroPak-15a Serial Port Pin-Out Descriptions
Connector
Pin No.
a
COM1
COM2
N/C
1
2
3
4
5
6
7
8
9
Reserved
RXD1
RXD2
TXD2
TXD1
N/C
Reserved
GND
GND
Reserved
RTS1
N/C
RTS2
CTS2
N/C
CTS1
Reserved
a.The internal COM3 port is labelled
COM2 on the EuroPak-15a.
Table 54: EuroPak-15a I/O Port Pin-Out Descriptions
Signal
Connector Pin No.
Signal Descriptions
Name
Reserved
PPS
1
2
3
4
5
6
7
8
9
Pulse per second
MSR
Measure output
Mark input
MKI
PV
Valid position available
Reserved
RESETOUT Reset output to an external system, active high
ERROR
GND
Indicates a fatal error when high
Digital ground
114
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Technical Specifications
Appendix A
A.1.2 Cables
A.1.2.1
12V Power Adapter Cable (NovAtel part number 01017023)
The power adapter cable supplied with the EuroPak-15a, see Figure 16, provides a convenient means for
supplying +12 VDC while operating in the field.
Input is provided through the standard 12V power outlet. The output from the power adapter utilizes a 4-pin
LEMO connector (LEMO part number FGG.0B.304.CLAD52Z) and plugs directly into the PWR input located
on the back panel of the EuroPak-15a.
9
1 (-)
4 (-)
2 (+)
3 (+)
10
1
2
3
4
-
5
6
+
+ 7
-
8
11
12
13
Reference
Description
Reference
Description
1
2
3
4
Black
Red
Orange
Brown
5
6
7
8
Ground
+9 to +18 VDC
+9 to +18 VDC
Ground
9
10
11
Connector key marking
12V adapter
Spring
12
13
Universal tip
6 Amp slow-blow fuse
Figure 16: EuroPak-15a Power Cable
EuroPak-15a Receiver User Manual Rev 5
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Appendix A
Technical Specifications
A.1.2.2
Null-Modem Cable (NovAtel part number 60323062)
This cable supplied with the EuroPak-15a, see Figure 17, provides an easy means of communications with a
PC. The cable is equipped with a 9-pin connector at the receiver end which can be plugged into the COM1,
COM2, or AUX port. At the PC end, a 9-pin connector is provided to accommodate a PC serial (RS232)
communication port.
1
5
5
1
6
9
9
6
11
Wiring Table:
Connector
Pin Number
To DB9S (10)
To DB9S (11)
2
3
3
2
8
7
7
8
4
5
5
1 & 6
1 & 6
4
Reference
Description
10
11
DB9S (Female)
DB9S (Female)
Figure 17: EuroPak-15a Null Modem Cable
116
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Technical Specifications
A.1.2.3 Straight Through Serial Cable (NovAtel part number 60723066)
Appendix A
This cable can be used to connect the EuroPak-15a to a modem or radio transmitter to propagate differential
corrections. The cable is equipped with a female DB9 connector at the receiver end. The male DB9 connector
at the other end is provided to plug into your user-supplied equipment (please refer to your modem or radio
transmitter user guide for more information on its connectors). The cable is approximately 2 m in length. See
1
5
1
5
9
6
6
9
11
1
2
3
4
5
6
7
8
9
1
2
3
4
5
6
7
8
9
Reference
Description
Reference
Description
9-conductor cable
10
11
DB9P (male) connector
DB9S (female) connector
12
Figure 18: EuroPak-15a Straight Through Serial Cable
EuroPak-15a Receiver User Manual Rev 5
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Appendix A
Technical Specifications
A.1.2.4
I/O Strobe Port Cable (NovAtel part number 60723065)
The strobe lines on the EuroPak-15a can be accessed by inserting the male DB9 connector of the I/O strobe
port cable into the I/O port. The other end of this cable is provided without a connector to provide flexibility.
The jacket insulation is cut away slightly from the end but the insulation on each wire is intact. The cable is
1
5
9
6
1
2
3
4
5
6
7
8
9
Wiring Table:
I/O Port
Pin
I/O Port
Signal
I/O Port Cable
Wire Color
I/O Port
Pin
I/O Port
Signal
I/O Port Cable
Wire Color
1
2
3
4
5
VARF
Black
Brown
Red
6
7
8
9
Reserved
Reserved
GND
Green
PPS
Blue
Reserved
Event1
PV
Violet
Orange
Yellow
GND
White/Grey
Reference
Description
Reference
Description
9-conductor cable
10
DB9P (male) connector
11
Figure 19: EuroPak-15a I/O Strobe Port Cable
118
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Appendix A
Technical Specifications
A.2 Channel Assignments
Table 55: 10GALILEO6GPS Channel Configuration
Signal
Channel
SV
Channel
Symbol
Rate
Sky
Search
SV Type Code DLL Type
Frame
Nav Type
FEC
0
1
2
3
4
5
6
7
8
0
1
2
3
4
5
6
7
8
Galileo
L1
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
Galileo
250
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
No
Galileo
Galileo
Galileo
Galileo
Galileo
L1
L1
L1
Galileo
Galileo
Galileo
Galileo
Galileo
250
250
250
250
50
50
50
50
L1
E5a
E5a
E5a
E5a
E5a
L1 C/A
Galileo
Galileo
Galileo
Galileo
GPS
GPS
GPS
GPS
GPS
Galileo
Galileo
Galileo
Galileo
GPS
GPS
GPS
GPS
GPS
9
9
50
50
50
50
50
50
50
10
11
12
13
14
15
10
11
12
13
14
15
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
No
No
No
No
No
GPS
GPS
Table 56: 16GPSL1L5 Channel Configuration
Signal
Channel
SV
Channel
Symbol
Rate
Sky
Search
SV Type Code DLL Type
Frame
Nav Type
FEC
0
1
2
3
4
5
6
7
8
0
1
2
3
4
5
6
7
8
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
50
50
50
50
50
50
50
50
100
100
100
100
100
100
100
100
No
No
No
No
No
No
No
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
9
9
10
11
12
13
14
15
10
11
12
13
14
15
120
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Technical Specifications
Appendix A
Table 57: 16GALILEOL1E5a Channel Configuration
Symbol
Signal
Channel
SV
Channel
Sky
Search
SV Type Code DLL Type
Frame
Nav Type
FEC
Rate
0
1
2
3
4
5
6
7
8
0
1
2
3
4
5
6
7
8
Galileo
L1
L1
L1
L1
L1
L1
L1
L1
E5a
E5a
E5a
E5a
E5a
E5a
E5a
E5a
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
Galileo
250
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
250
250
250
250
250
250
250
50
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
9
9
50
50
50
50
50
50
50
10
11
12
13
14
15
10
11
12
13
14
15
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Galileo
Table 58: 12GPS4GEOL1L5 Channel Configuration
Symbol
Signal
Channel
SV
Channel
Sky
Search
SV Type Code DLL Type Frame Nav Type
FEC
Rate
0
1
2
3
4
5
6
7
8
0
1
2
3
4
5
6
7
8
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GEO
GEO
GEO
GEO
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
WAAS
WAAS
WAAS
WAAS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
WAAS
WAAS
WAAS
WAAS
50
50
50
50
50
50
100
100
100
100
100
100
500
500
500
500
No
No
No
No
No
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Idle
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
9
9
10
11
12
13
14
15
10
11
12
13
14
15
L1 C/A Standard
L1 C/A
L5 C5
L5 C5
Narrow
Narrow
Narrow
Idle
Idle
Idle
EuroPak-15a Receiver User Manual Rev 5
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Appendix A
Technical Specifications
Table 59: 8GPS8GEO Channel Configuration
SV Type Code DLL Type Frame Nav Type
Signal
Channel
SV
Channel
0
Symbol
Rate
FEC Sky Search
0
1
2
3
4
5
6
7
8
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GEO
GEO
GEO
GEO
GEO
GEO
GEO
GEO
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
L1 C/A
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
WAAS
WAAS
WAAS
WAAS
WAAS
WAAS
WAAS
WAAS
50
50
50
50
50
50
50
50
500
500
500
500
500
500
500
500
No
No
No
No
No
No
No
No
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Idle
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
L1 C/A Standard WAAS
L1 C/A Standard WAAS
9
Idle
Idle
10
11
12
13
14
15
L1 C/A
L1 C/A
L5 C5
L5 C5
L5 C5
L5 C5
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
WAAS
WAAS
WAAS
WAAS
WAAS
WAAS
Idle
Idle
Idle
Idle
Idle
Table 60: 16GPSL5 Channel Configuration
Signal
Channel
0
SV
Channel
0
Symbol
Rate
SV Type Code DLL Type Frame Nav Type
FEC Sky Search
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
L5 C5
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
Narrow
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
GPS
100
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Yes
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
Auto
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
122
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Appendix B Electrostatic Discharge Control (ESD)
Practices
B.1 Overview
Static electricity is electrical charge stored in an electromagnetic field or on an insulating body. This charge can
flow as soon as a low-impedance path to ground is established. Static-sensitive units can be permanently
damaged by static discharge potentials of as little as 40 volts. Charges carried by the human body, which can be
thousands of times higher than this 40 V threshold, can accumulate through as simple a mechanism as walking
across non-conducting floor coverings such as carpet or tile. These charges may be stored on clothing,
especially when the ambient air is dry, through friction between the body and/or various clothing layers.
Synthetic materials accumulate higher charges than natural fibers. Electrostatic voltage levels on insulators
may be very high, in the order of thousands of volts.
Various electrical and electronic components are vulnerable to electrostatic discharge (ESD). These include
discrete components, hybrid devices, integrated circuits (ICs), and printed circuit boards (PCBs) assembled
with these devices.
B.2 Handling ESD-Sensitive Devices
ESD-sensitive devices must only be handled in static-controlled locations. Some recommendations for such
handling practices follow:
•
•
•
Handling areas must be equipped with a grounded table, floor mats, and wrist strap.
A relative humidity level must be maintained between 20% and 80% non-condensing.
No ESD-sensitive board or component should be removed from its protective package, except in
a static-controlled location.
•
•
•
•
A static-controlled environment and correct static-control procedures are required at both repair
stations and maintenance areas.
ESD-sensitive devices must be handled only after personnel have grounded themselves via wrist
straps and mats.
Boards or components should never come in contact with clothing, because normal grounding
cannot dissipate static charges on fabrics.
A circuit board must be placed into an anti-static plastic clamshell before being removed from the
work location and must remain in the clamshell until it arrives at a static-controlled repair/test
center.
•
•
Circuit boards must not be changed or moved needlessly. Handles may be provided on circuit
boards for use in their removal and replacement; care should be taken to avoid contact with the
connectors and components.
On-site repair of ESD-sensitive equipment should not be undertaken except to restore service in
an emergency where spare boards are not available. Under these circumstances repair station
techniques must be observed. Under normal circumstances a faulty or suspect circuit board must
be sent to a repair center having complete facilities, or to the manufacturer for exchange or repair.
•
•
Where protective measures have not been installed, a suitable alternative would be the use of a
Portable Field Service Grounding Kit (for example, 3M Kit #8501 or #8507). This consists of a
portable mat and wrist strap which must be attached to a suitable ground.
A circuit board in a static-shielding bag or clamshell may be shipped or stored in a cardboard
carton, but the carton must not enter a static-controlled area such as a grounded or dissipative
bench top or repair zone. Do not place anything else inside the bag (for example, repair tags).
•
•
Treat all PCBs and components as ESD sensitive. Assume that you will damage the PCB or
component if you are not ESD conscious.
Do not use torn or punctured static-shielding bags. A wire tag protruding through the bag could act
as a "lightning rod", funneling the entire charge into the components inside the bag.
•
•
Do not allow chargeable plastics, such as binders, within 0.6 m of unshielded PCBs.
Do not allow a PCB to come within 0.3 m of a computer monitor.
EuroPak-15a Receiver User Manual Rev 5
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Appendix B
Electrostatic Discharge Control (ESD) Practices
B.3 Prime Static Accumulators
Table 61: Static-Accumulating Materials
•
•
•
•
formica (waxed or highly resistive)
finished wood
synthetic mats
Work Surfaces
writing materials, note pads, and so on
•
•
wax-finished
vinyl
Floors
•
•
•
common cleanroom smocks
personal garments (all textiles)
non-conductive shoes
Clothes
•
•
•
finished wood
vinyl
fiberglass
Chairs
•
•
•
common polyethylene bags, wraps, envelopes, and bubble pack
pack foam
common plastic trays and tote boxes
Packing and
handling
•
•
•
•
•
spray cleaners
common solder sucker
common soldering irons
common solvent brushes (synthetic bristles)
cleaning, drying and temperature chambers
Assembly,
cleaning, and
repair areas
B.4 Handling Printed Circuit Boards
ESD damage to unprotected sensitive devices may occur at any time. ESD events can occur far below the
threshold of human sensitivity. Follow this sequence when it becomes necessary to install or remove a circuit
board:
1. After you are connected to the grounded wrist strap, remove the circuit board from the frame and place it
on a static-controlled surface (grounded floor or table mat).
2. Remove the replacement circuit board from the static-shielding bag or clamshell and insert it into the
equipment.
3. Place the original board into the shielding bag or clamshell and seal it with a label.
4. Do not put repair tags inside the shielding bag or clamshell.
5. Disconnect the wrist strap.
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Appendix C Standards/References
GPS L5 SIGNAL SPECIFICATION REFERENCE
For copies of the Interface Control Document (ICD)-GPS-705, contact:
ARINC Research Corporation
Address:
2551 Riva Road
Annapolis, MD, USA
21401-7465
Telephone:
Fax:
410-266-4000
410-266-4049
Website:
GEODETIC SURVEY OF CANADA
Geodetic Survey of Canada
Address:
615 Boothe Street
Ottawa, ON, Canada
K1A 0E9
Telephone:
Fax:
(613) 995-4410
(613) 995-3215
Website:
U.S. NATIONAL GEODETIC SURVEY
NGS Information Services
Address:
1315 East-West Highway
Station 9244
Silver Springs, MD, USA
20910-3282
Telephone:
Fax:
(301) 713-2692
(301) 713-4172
Website:
ꢀ Contact information may be subject to change however they are accurate at the time of publication.
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Appendix D Replacement Parts
The following are a list of the replacement parts available for your NovAtel GPS receiver. Should you require
assistance or need to order additional components, please contact your local NovAtel dealer or Customer
Service representative.
D.1 EuroPak-15a
Part Description
NovAtel Part
60723065
60723066
60715062
01017023
D.2 Accessories
Part Description
Aviation Compact Disc with PC utilities
NovAtel Part
01017679
C006
Optional RF Antenna Cables:
5 meters
15 meters
C016
30 meters.
C032
22 cm interconnect adapter cable
GPS-C002
D.3 Manufacturer’s Part Numbers
The following original manufacturer’s part numbers, for the EuroPak-15a cables, are provided for information
only and are not available from NovAtel as separate parts:
Part Description
LEMO Part
FGG.0B.304.CLAD52Z
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Index
automatic channel assignment
A
accuracy
B
acquisition
Binary
binary
almanac
ambiguity
antenna
C
cables
channel
ASCII
assign
atmosphere
control
clock
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Index
D
data
COM port
differential corrections
distance
Doppler
commands
communication
configuration
E
configuring
elevation
cut-off angle
control
ephemeris
errors
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Index
I
F
fields
filter
firmware
L
latitude
logs
G
GPS
longitude
H
hardware
M
memory
message
model
health
height
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Index
position
N
noise
processing
note
O
offset
Q
R
range
overview
receiver
P
phase-lock-loop
ports
response messages
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Index
T
threshold
time
S
satellite
SBAS
satellites
TIME port
tracking
setting
types
specifications
start up
status
steer
U
unassign
unlog
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Index
V
velocity
W
week
Y
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Index
EuroPak-15a Receiver User Manual Rev 5
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Recyclable
Printed in Canada on recycled paper
OM-20000100
Rev 5
2007/04/26
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