Novatel OM-20000077 RTCM2 Delta Differential GPS Corrections Fixed, Chapter Message Formats

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Chapter 5

Message Formats

computed by the base station generating this Type 1 message. The message is of variable length, depending on the number of satellites visible and pseudoranges corrected by the base station. Satellite specific data begins at word 3 of the message.

Type 1 messages contain the following information for each satellite in view at the base station:

Satellite ID

Pseudorange correction

Range-rate correction

Issue of Data (IOD)

When operating as a base station, the receiver’s position must be set using Message ID# 80, Set User’s Position/Operating Mode. When operating as a rover station, the receiver COM port receiving the RTCM data must be set to Rover mode using command Message ID# 80. Please refer to the L1 GPS Firmware Reference Manual for more details on this input message.

5.1.2RTCM2 Delta Differential GPS Corrections (Fixed)

Quite often a base station may have new ephemeris data before rover stations have collected the newer ephemeris. The purpose of Type 2 messages is to act as a bridge between old and new ephemeris data. A base station will transmit this Type 2 bridge data concurrently with Type 1's for a few minutes following receipt of a new ephemeris. The rover station adds the Type 2 data (delta of old ephemeris minus new ephemeris) to the Type 1 message data (new ephemeris) to calculate the correct pseudorange corrections (based on the old ephemeris). Once the rover receiver has collected its own updated ephemeris, it will no longer utilize the Type 2 messages.

The GPS Card will accept and decode RTCM Standard Type 2 messages, when available and if required.

Type 2 messages are variable in length, depending on the number of satellites being tracked by the base station.

5.1.3RTCM9 Partial Satellite Set Differential Corrections

RTCM Type 9 messages follow the same format as Type 1 messages. However, unlike a Type 1 message, Type 9 does not require a complete satellite set. This allows for much faster differential correction data updates to the rover stations, thus improving performance and reducing latency.

Type 9 messages should give better performance with slow or noisy data links.

The base station transmitting the Type 9 corrections must be operating with a high-stability clock to prevent degradation of navigation accuracy due to the unmodeled clock drift that can occur between Type 9 messages. For this reason, only receivers with an external oscillator can generate Type 9 messages. SUPERSTAR II receivers can accept Type 9 messages.

NovAtel recommends a high-stability clock such as the PIEZO Model 2900082 whose 2-sample (Allan) variance meets the following stability requirements:

3.24 x 10-24s2/s2 between 0.5 - 2.0 seconds, and 1.69 x 10-22T s2/s2 between 2.0 - 100.0 seconds

An external clock, such as an OCXO, requires approximately 10 minutes to warm up and become fully stabilized after power is applied; do not broadcast RTCM Type 9 corrections during this warm-up period.

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SUPERSTAR II User Manual Rev 3

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Contents Superstar Proprietary Notice Table of Contents Appendices Tables Figures Software License Software License Firmware Updates Contact InformationElectrostatic Discharge CE Notice Warranty Policy Congratulations Scope Related PublicationsRelated Publications Introduction Superstar II GPS CardFlexPak-SSII Introduction ChapterChapter Introduction Receiver Specifications Physical CharacteristicsSystem Architecture Radio Frequency RF SectionEnclosure and Wiring Harness Principal Power SupplyOptional LNA Power Supply GPS AntennaInstallation Typical System Configuration Reference DescriptionChapter Installation Electrostatic DischargeEquipment Interconnection Serial ConnectionInstallation Considerations Power ConnectionInstallation Chapter Antenna LocationConnectors and Connector Pins Assignment 1 J1 Interface and Power ConnectorData Link Base Station and Rover Units SeparationRF Connector J2 Serial Data InterfacePreamplifier Power Pass-Through Antenna Supply Protocol Selection and Non Volatile MemoryMemory Back-Up RF InputUse of Discretes Discretes IP2 and IP3 functionsDefault Configuration Non Volatile MemoryNon-Volatile Memory Data Installation Overview Description ReferenceTypical Operational Configuration Reference Description OperationSerial Port Default Settings Communications with the ReceiverGetting Started Operation ChapterPower-Up Information Boot InformationOperational Information Chapter OperationConfigurable Parameters Data RequestsReceiver States Self-Test Mode Dead-Reckoning Mode Built-In Status TestsDatum Support Message Formats RTCM-Format MessagesRTCM1 Differential GPS Corrections Fixed RTCM2 Delta Differential GPS Corrections Fixed RTCM9 Partial Satellite Set Differential CorrectionsChapter Message Formats Nmea Format Data Messages Message Formats ChapterGPS System Errors Positioning Modes of OperationSingle-Point or Autonomous Satellite-Based Augmentation System Sbas Positioning Modes of Operation ChapterSbas Receiver Sbas MessagesChapter Positioning Modes of Operation Positioning Modes of Operation Chapter Troubleshooting Cable Lengths Vs. GainTroubleshooting Chapter Technical Specifications Appendix aSuperstar II Family Performance Technical Specifications Appendix a Output MessagesAppendix a Technical Specifications Mechanical DrawingConnector Pin Assignment J1 Interfaces and Power Connector Pin Assignment3 I/O Electrical Characteristics O Signals Voltage LimitsFlexPak-SSII Specifications Appendix BStatus Indicators Appendix B FlexPak-SSII SpecificationsFlexPak Status Indicators Port Pin-OutsFlexPak-SSII Specifications Appendix B Automobile Power Adapter Cable NovAtel part numberCables 3.2 13-Pin Deutsch to DB9 Serial Cable NovAtel part number FlexPak 13-Pin Serial CableSetup and Operation Normal SetupDevelopment Kit DescriptionDgps Setup with the FlexPak-SSII Differential GPS SetupStarView Software Installation Antenna Specifications Coaxial Cable SpecificationsAppendix C Cable SelectionAntenna Specifications Appendix C Geodetic Active AntennaAntenna Gain Depending on Cable Length Required Typical Current Consumption Versus Antenna GainAppendix C Antenna Specifications Active AntennaPassive Antenna Recommended Geodetic Active AntennasPassive Antenna Specifications Patch Element GPS Antenna 201-990146-716 MCX, +12 dBGPS Antenna 201-990147-606 +26 dB Antenna Specifications Appendix C Appendix D Standards/ReferencesAppendix E Ttff and Satellite AcquisitionTime-To-First-Fix Ttff Re-AcquisitionUtility Installation Appendix FUpdating Receiver Firmware System RequirementsStarting Software and Options Update Registration Key AcceptedUpdating Receiver Firmware Appendix F Programming Success Appendix F Updating Receiver FirmwareAppendix G GPS OverviewGPS System Design Space SegmentHeight Relationships Control SegmentUser Segment Appendix G GPS OverviewGPS Positioning GPS Overview Appendix GSingle-Point vs. Relative Positioning Accuracy versus Precision1Multipath Static vs. Kinematic PositioningReal-time vs. Post-mission Data Processing Why Does Multipath Occur? Consequences of Multipath ReceptionHardware Solutions For Multipath Reduction Antenna Site SelectionGPS Signal Multipath vs. Increased Antenna Height Antenna DesignsGPS Overview Appendix G Appendix H Glossary of TermsGlossary of Terms Appendix H Appendix H Glossary of Terms Glossary of Terms Appendix H Appendix AcronymsAcronyms Appendix Appendix Acronyms Index GEO, Sbas IndexIndex Index OM-20000077 Rev 2004/03/11