Tri-M Systems FV-25 User Manual

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1
Tri-M Systems, Inc.
Unit 100, 1407 Kebet way
Port Coquitlam, BC V3C 6L3
Canada
www.tri-m.com
Phone: 604.945.9565
Fax: 604.945.9566
info@tri-m.com
FV – 25
USER’S GUIDE
This document features the specification of FV-25 and describes the details on using the evaluation kit
to evaluate the performance of FV-25 and select the desired functions. It intends to help users to obtain
the maximum performance from FV-25 in users’ integrating GPS systems.
Version: 1.0
Date: January 2005
Page view 0
1 2 3 4 5 6 ... 157 158

Summary of Contents

Page 1 - FV – 25

1Tri-M Systems, Inc. Unit 100, 1407 Kebet wayPort Coquitlam, BC V3C 6L3 Canadawww.tri-m.com Phone: 604.945.9565 Fax: 604.945.9566 [email protected] FV

Page 2 - Contents

10Specification Performance Characteristics Receiver Type L1 frequency, C/A code, 16 Channels Position Accuracy w

Page 3

1002 U1 Reserved 3 U1 Inverse_flags Bit 0 – invert meaning of direction pin; 0: High=Forwards; 1: High=Backwards Bit 1 – invert meaning of gyr

Page 4 - List of Figures

101UBX Class INF Basically, the INF class is an output class. It outputs strings with a printf-style call. INF – ERROR (0x04 0x00) It outputs an ASC

Page 5 - List of Tables

102INF – WARNING (0x04 0x01) It outputs an ASCII string to indicate warning message. Header ID Data Length Data Checksum 0xB5 0x62 0x04 0x01 N*1

Page 6 - Preface

103INF – NOTICE (0x04 0x02) It outputs an ASCII string to transmit informational contents. Header ID Data Length Data Checksum 0xB5 0x62 0x04 0x02

Page 7

104INF – TEST (0x04 0x03) It outputs an ASCII string to indicate test message. Header ID Data Length Data Checksum 0xB5 0x62 0x04 0x03 N*1 See be

Page 8 - Chapter 1 Introduction

105INF – DEBUG (0x04 0x04) It outputs an ASCII string to indicate debug message. Header ID Data Length Data Checksum 0xB5 0x62 0x04 0x04 N*1 See

Page 9

106INF – USER (0x04 0x07) It outputs an ASCII string to indicate user output message. Header ID Data Length Data Checksum 0xB5 0x62 0x04 0x07 N*1

Page 10

107UBX Class MON This message is used to transmit GPS receiver status, such as CPU status, I/O status, etc.. MON – SCHD (0x0A 0x01) It periodically

Page 11 - Antenna

108MON – IO (0x0A 0x02) It periodically polls the I/O status. Header ID Data Length Data Checksum 0xB5 0x62 0x0A 0x02 80 See below CK_A CK_B Da

Page 12 - Chapter 2 Start

109MON – MAGPP (0x0A 0x06) It periodically polls message parse and process status. Header ID Data Length Data Checksum 0xB5 0x62 0x0A 0x06 144 Se

Page 13 - Pin Definitions

11Dimension 37.1mm x 25.6 mm Thickness 3.9 mm Weight 9.5 g (include an S

Page 14

110MON – RXBUF (0x0A 0x07) It periodically polls the status of receiver buffer. Header ID Data Length Data Checksum 0xB5 0x62 0x0A 0x07 16 See be

Page 15

111MON – TXBUF (0x0A 0x08) It periodically polls the status of transmitter buffer. Header ID Data Length Data Checksum 0xB5 0x62 0x0A 0x08 20 See

Page 16

112MON – VER (0x0A 0x04) It is used to poll the hardware/software version. Header ID Data Length Data Checksum 0xB5 0x62 0x0A 0x04 40+N*30 See be

Page 17

113UBX Class NAV The messages in this class transmit navigation data, status flags, and accuracy information. NAV – POSECEF (0x01 0x01) It periodica

Page 18

114NAV – POSLLH (0x01 0x02) It periodically polls the receiver’s position in the local geodetic frame. Header ID Data Length Data Checksum 0xB5 0x62

Page 19

115NAV – POSUTM (0x01 0x08) It periodically polls the receiver’s position in the UTM frame. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x08

Page 20

116NAV – DOP (0x01 0x04) It periodically polls the values of DOPs. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x04 18 See below CK_A CK_

Page 21

117NAV – STATUS (0x01 0x03) It periodically polls navigation status. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x03 16 See below CK_A C

Page 22 - Figure 2.13 Tracking View

118NAV – SOL (0x01 0x06) It periodically polls the information about navigation solution. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x06

Page 23

119NAV – VELECEF (0x01 0x11) It periodically polls velocity solution in the ECEF frame. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x11 20

Page 24 - Figure 2.17 Restart

12 Chapter 2 Start 2.1 Pin Definitions and Reference Layout Figure 2.1 shows the pin definitions of FV-25. Table 2.1 describes the corresponding def

Page 25 - Figure 2.18 DGPS

120NAV – VELNED (0x01 0x12) It periodically polls velocity solution in the NED frame. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x12 36

Page 26 - Chapter 3 Alternative Start

121NAV – TIMEGPS (0x01 0x20) It periodically polls the information about GPS time. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x20 16 See

Page 27

122NAV – TIMEUTC (0x01 0x21) It periodically polls the information about UTC time. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x21 20 See

Page 28

123NAV – CLOCK (0x01 0x22) It periodically polls receiver clock information. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x22 20 See below

Page 29 - Chapter 4 Navigation

124NAV – SVINFO (0x01 0x30) It periodically polls the information about UTC time. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x30 8+N*12

Page 30

125NAV – DGPS (0x01 0x31) It periodically polls DGPS correction data that are used in the navigation solution. Header ID Data Length Data Checksum 0

Page 31

126NAV – SBAS (0x01 0x32) It periodically polls the status of SBAS. Header ID Data Length Data Checksum 0xB5 0x62 0x01 0x32 12+N*12 See below CK

Page 32

12717+N*12 U1 Reserved 18+N*12 I2 Pseudo range correction (cm) 20+N*12 I2 Reserved 22+N*12 I2 Ionosphere correction (cm)

Page 33

128UBX Class RXM This class transmits the status of receiver manager and received raw data, e.g. pseudorange and carrier phase measurements, ephemeri

Page 34

129RXM – SFRB (0x02 0x11) It periodically outputs the data in the subframe of navigation message. Header ID Data Length Data Checksum 0xB5 0x62 0x0

Page 35 - Chapter 5 Evaluation Kit

13Pin Definitions Pin No. Title I/O Note a VIN-1 I Voltage input 5~12V DC (MUST leave open if VIN-2 is used)b VANT I Antenna bias voltage input DC

Page 36

130RXM – SVSI (0x02 0x20) It periodically polls the information of SV status. Header ID Data Length Data Checksum 0xB5 0x62 0x02 0x20 8+N*6 See b

Page 37

131RXM – ALM (0x02 0x30) It’s an input request for polling almanac data. The receiver responds with all available (32) RXM-ALM messages defined below

Page 38 - Chapter 6 Antennas

132not valid. 2. WORD0 ~ WORD7 contain the data following the Hand-Over Word (HOW) in the navigation message. The data are from the sub-frame 4 of Pa

Page 39

133RXM – EPH (0x02 0x31) It’s an input request for polling ephemeris data. The receiver responds with all available RXM-EPH messages defined below.

Page 40

13436+n*96 U4 Sub-frame 1 – WORD7 40+n*96 U4 Sub-frame 2 – WORD0 44+n*96 U4 Sub-frame 2 – WORD1 48+n*96 U4 Sub-frame 2 – WORD2 52+n*9

Page 41

135RXM – POSREQ (0x02 0x40) It’s an input message for requesting a position fix in the FixNow mode (power saving mode). Header ID Data Length Data C

Page 42

136UBX Class TIM This class transmits the information of time pulse and time mark. TIM – TM (0x0D 0x02) It periodically polls the time mark data. H

Page 43

137TIM – TP (0x0D 0x01) It periodically polls the time pulse data. Header ID Data Length Data Checksum 0xB5 0x62 0x0D 0x01 16 See below CK_A CK_

Page 44

138UBX Class UPD This class is used to update the firmware. UPD – DOWNL (0x09 0x01) It is an I/O message. It is used to download data to memory. He

Page 45

139UPD – UPLOAD (0x09 0x02) It is an I/O message. It is used to upload data from memory. Header ID Data Length Data Checksum 0xB5 0x62 0x09 0x02 1

Page 46

14 2.2 Sanav_Demo Sanav_Demo is required to run on a PC with at least 4 MB RAM and Windows 98 that has at least one available serial comm. port (fr

Page 47

140 Chapter 8 Troubleshooting The following table lists questions/problems that you might encounter for operating the module and possible suggested

Page 48

1416. The estimated positions have steadily expressed about a few meters or up to a few hundred meters off the reference position. Make sure the esti

Page 49

142 Appendix A Geodetic ID: Coordinate Datum Index Name Acronym DX (m) DY(m) DZ (m) Ellipsoid Index (See below) Rotation and Scale (See bel

Page 50

14318 ARC 1950 - Zambia ARF-F -147.0 -74.0 -283.0 7 0 19 ARC 1950 - Zimbabwe ARF-G -142.0 -96.0 -293.0 7 0 20 ARC 1960 - Mean (Kenya, T

Page 51

14441 Djakarta (Batavia)- Sumatra (Indonesia) BAT -377.0 681.0 -50.0 5 0 42 Hong Kong 1963 - Hong Kong HKD -156.0 -271.0 -189.0 20 0 43

Page 52

14562 Tokyo - Okinawa TOY-C -158.0 507.0 676.0 5 0 63 Tokyo - South Korea TOY-B -146.0 507.0 687.0 5 0 64 Australian Geodetic 1966 - Au

Page 53

14680 European 1979 - Mean Solution (AU, FN, NL, N, E, S, CH) EUS -86.0 -98.0 -119.0 20 0 81 Hjorsey 1955 - Iceland HJO -73.0 46.0 -86.0

Page 54

147Alaska (excluding Aleutian Islands) 96 N. American 1927 - Aleutian Islands, East of 180W NAS-V -2.0 152.0 149.0 6 0 97 N. American 1927

Page 55

148Caribbean 108 N. American 1927 - Central America NAS-N 0.0 125.0 194.0 6 0 109 N. American 1927 - Cuba NAS-T -9.0 152.0 178.0 6 0 110

Page 56

149Bolivia 124 Prov S. American 1956 - Northern Chile (near 19S) PRP-B -270.0 183.0 -390.0 20 0 125 Prov S. American 1956 - Southern Chile

Page 57

15Figure 2.4 Setting of comm. port number. For setting the value of baud rate, pull the scroll-down window for the “Baud rate” item and the desired

Page 58

150Galapagos Islands) 139 South American 1969 - Baltra, Galapagos Islands SAN-J -47.0 26.0 -42.0 22 0 140 South American 1969 - Guyana SAN-

Page 59

151154 L.C. 5 Astro 1961 - Cayman Brac Island LCF 42.0 124.0 147.0 6 0 155 Montserrat Island Astro 1958 - Montserrat Leeward Islands ASM

Page 60

152Diego Garcia 169 Kerguelen Island 1949 - Kerguelen Island KEG 145.0 -187.0 103.0 20 0 170 Mahe 1971 - Mahe Island MIK 41.0 -220.0 -13

Page 61

153185 Johnston Island 1961 - Johnston Island JOH 189.0 -79.0 -202.0 20 0 186 Kusaie Astro 1951 - Caroline Islands, Fed. States of Micronesia

Page 62

154Antarctica 202 European 1950 - Iraq, Israel, Jordan, Kuwait, Lebanon, Saudi Arabia & Syria EUR-S -103.0 -106.0 -141.0 20 0 203 Gunung

Page 63

155Ellipsoids Index Name Semi Major Axis (m) 1/Flattening 0 WGS 84 6378137.000 298.257223563 1 Airy 1830 6377563.396 299.3249646 2 Modified Air

Page 64

156Rotation and Scale Table Index Name Rot. X (seconds) Rot. Y (seconds) Rot. Z (seconds) Scale (-) 0 +0.0000 +0.0000 +0.0000 0.0001 0.0000 0.

Page 65

157 Appendix B Acronyms BBR Battery Backed-up RAM CLT Carrier Lock Time CN0 Carrier to Noise Ratio COG Course Over Ground CTM Conti

Page 66

158 References 1. ANTARISR Chipset – System Integration- Manual for San Jose Navigation, Doc. No. GPS.G3-DK-03014. 2. ANTARISR Protocol Specificatio

Page 67

16subsequent window will be the one shown in Figure 2.6, i.e., the navigation data from the module are displayed in the corresponding sub-windows. If

Page 68 - Message not-acknowledged

17 Figure 2.7 Constellation Map of GPS satellites. 2.2.4 Message View for NMEA Messages Figure 2.8 is the window for showing the desired (user-selec

Page 69

18accumulatively within the sub-window until the sub-window is filled up, i.e., the “Message View” window contains NMEA messages from several epochs,

Page 70

19Figure 2.10 Available NMEA messages. NOTE: The output NMEA messages will be discarded or not transmitted if the values of the baud rate is not su

Page 71

2Contents Preface………………………………………………………… Chapter 1 Introduction……………………………………….. 1.1 Supports……………………………………………………….. Chapter 2 Start…………………………………

Page 72

20Figure 2.11 GPS satellite information. 2.2.7 Receiver Information Figure 2.12 describes the receiver information. They are: UTC Date: day/month/y

Page 73

21Figure 2.12 Receiver Information. NOTE: Data displayed in the sub-windows (Figures 2.7, 2.9, 2.11, and 2.12) depend on the user-selected output NM

Page 74

22Figure 2.13 Tracking View. 2.2.9 User Setting Clicking “Windows/User Setting” or the shortcut button ?, the “User Setting” window is activated, as

Page 75 - 36 U4 Almanac – WORD7

23 The output position will be updated as the position is fixed. 2.2.9.2 Time and day This function sets the initial UTC date and time, as shown in

Page 76

24Figure 2.16 Local time zone. 2.2.9.4 Restart This function sets the initial start-up mode, such as cold-start, warm-start, and hot-start, for the

Page 77

252.2.9.5 DGPS This function activates the differential GPS functions of the module, such as RTCM and WAAS/EGNOS, or only GPS function without aids,

Page 78

26 Chapter 3 Alternative Start This chapter introduces an alternative utility, HyperTerminal (from Windows), to display the NMEA information. And, U

Page 79

27the mode of connection. Figure 3.2 Connection settings. After setting all the necessary data, click the connection button, which is the fifth sho

Page 80

28will ask users to input the file name and folder. 3.3 Setting Configuration or Polling Information from Module For setting or polling the desired

Page 81

29 Chapter 4 Navigation 4.1 Operating Modes 4.1.1 Continuous Tracking Mode (CTM) CTM is the default setting of the module. While the CTM is on, the

Page 82

3 4.5 Navigation Data……………………………………………………. 4.5.1 Position Format……………………………………………… 4.5.2 Datums………………………………………………………. 4.5.3 Update Rate…………………

Page 83

30 Conditions Modes Time Position Almanac Ephemeris Cold Start None None None None Warm Start Yes Yes Yes None Hot Start Yes Yes Yes Yes Tab

Page 84

31will improve on TTFF depends on the accuracy of position and time from a near base station (service center) as well as hardware synchronization. T

Page 85

32dB is used, the “High Sensitivity” mode is not recommended. 4.5 Navigation Data 4.5.1 Position Format The navigation data can be output in the for

Page 86

33initial/assumed value of the altitude is 500 m. If the 2D position fix occurs after the 3D position fix (number of observable satellites drops from

Page 87

34RTCM protocol, please refer to the web site http://www.rtcm.org/. The DGPS parameters can be changed in the UBX-CFG-NAV message, like DGPS Timeta

Page 88

35 Chapter 5 Evaluation Kit The evaluation kit is an optional accessory while purchasing the module. It will provide an easy way to estimate the per

Page 89 - the origin – Y axis

36re-start up the GPS module in the either Continuous Tracking Mode or FixNow mode. Figure 5.2 Front panel of the evaluation kit. Figure 5.3 s

Page 90

37Both Comm. ports are the bi-directional ports, i.e., the ports also accepts user software commands. For receiving RTCM message, either port can be

Page 91

38 Chapter 6 Antennas To get the maximum performance from the module, in addition to the own properties of the module, one of the important factors

Page 92

39For using passive antennas, the pin VANT (DC bias voltage) on the module is connected to ground, and the antenna is directly connected to the GPS s

Page 93 - CFG – RST (0x06 0x04)

4List of Figures Figure 2.1 FV-25 Pin definitions (Top View)………………………………….. Figure 2.2 A reference layout for FV-25……………………………………….. Figure 2.3 Setti

Page 94

406.3 Active Antenna Supervisor - Short Circuit Protection This is a built-in function that is monitored by the BaseBand processor. If an abnormal cu

Page 95

41 Chapter 7 Available NMEA and UBX Messages 7.1 NMEA Protocol The NMEA protocol expresses the data in the format of ASCII. This is a standard forma

Page 96

42the “PDOP Accuracy Mask”.

Page 97

43GGA – GPS Fix Data Position fix related data, such as position, time, number of satellites in use, etc.. $GPGGA,gga1,gga2,gga3,gga4,gga5,gga6,gga7

Page 98

44GLL – Geographic Position – Latitude/Longitude Navigation data and status. $GPGLL,gll1,gll2,gll3,gll4,gll5,gll6,gll7*hh<CR><LF> Param

Page 99

45GRS – GNSS Range Residual This message is used to monitor and support RAIM. $GPGRS,grs1,grs2,(grs3*12)*hh<CR><LF> Parameters Descript

Page 100

46GSA – GNSS DOP and Active Satellites Receiver operating mode, the values of DOPs, and PRN numbers for satellites used in the GGA position solution.

Page 101

47GST – GNSS Pseudorange Error Statistics This message is used to monitor and support RAIM. $GPGST,gst1,gst2,gst3,gst4,gst5,gst6,gst7,gst8*hh<CR&

Page 102 - INF – WARNING (0x04 0x01)

48GSV – GNSS Satellites in View This message indicates the observable satellites’ information, such as PRN numbers, elevation, azimuth, SNR, and numb

Page 103 - INF – NOTICE (0x04 0x02)

49RMC – Recommended Minimum Specific GNSS Data This message transmits the necessary navigation data, such as time, position, speed, course, and so on

Page 104 - INF – TEST (0x04 0x03)

5List of Tables Table 1.1 Specification of FV-25…………………………………………….. Table 2.1 Description of pin definition for FV-25…………………………… Table 4.1 Conditions

Page 105 - INF – DEBUG (0x04 0x04)

50TXT – Text Transmission The message is used to transmit short text messages. Transmitting a longer message needs multi-TXT messages. $GPTXT,txt1,t

Page 106 - INF – USER (0x04 0x07)

51VTG – Course Over Ground and Ground Speed This message transmits the speed and course relative to ground. $GPVTG,vtg1,vtg2,vtg3,vtg4,vtg5,vtg6,vtg

Page 107

52ZDA – Time & Date This message transmits UTC time and date, and local time zone. $GPZDA,zda1,zda2,zda3,zda4,zda5,zda6*hh<CR><LF>

Page 108 - MON – IO (0x0A 0x02)

53 7.1.2 Proprietary NMEA Messages The non-standard NMEA messages is proposed by u-blox. The proprietary (non-standard) NMEA messages are grouped int

Page 109 - MON – MAGPP (0x0A 0x06)

54PUBX, 00 – Latitude/Longitude Position Data Output message. This message transmits navigation data defined in the local geodetic frame. $PUBX,00,p

Page 110 - MON – RXBUF (0x0A 0x07)

55the position calculation p00x18 Number of GLONASS satellites used in the position calculation Always 0 p00x19 Dead reckoning used 0 – No; 1 – Ye

Page 111 - MON – TXBUF (0x0A 0x08)

56PUBX, 01 – UTM Position Data Output message. This message transmits navigation data defined in the Universal Transverse Mercator (UTM) frame. $PUB

Page 112 - MON – VER (0x0A 0x04)

57used in the position calculation p01x19 Dead reckoning used 0 – No; 1 – Yes hh Checksum hex number (2 – character) <CR><LF> End

Page 113

58PUBX,03 – Satellite Status Output message. $PUBX,03,p03x1,((p03x2,p03x3,p03x4,p03x5,p03x6,p03x7)*n)*hh<CR><LF> Parameters Description

Page 114 - NAV – POSLLH (0x01 0x02)

59PUBX,04 – Time of Day and Clock Information Output message. This message transmits UTC time, week number, and clock offset. $PUBX,04,p04x1,p04x2,p

Page 115

6 Preface The objective of The FV-25 User’s Guide is to help users to understand the properties of FV-25 thoroughly and, therefore, obtain the maxi

Page 116 - NOTE: All have Scaling 0.01

60GPQ – Poll Message Input message. Poll a standard NMEA message. $xxGPQ,gpq1*hh<CR><LF> Parameters Descriptions Notes $xxGPQ NMEA me

Page 117 - NAV – STATUS (0x01 0x03)

61PUBX – Poll a PUBX Message Input message. Poll the proprietary PUBX messages. $PUBX,p1*hh<CR><LF> Parameters Descriptions Notes p1

Page 118 - NAV – SOL (0x01 0x06)

62PUBX,40 – Set NMEA Message Output Rate Input message. $PUBX,40,p40x1,p40x2,p40x3,p40x4,p40x5*hh<CR><LF> Parameters Descriptions Note

Page 119 - NAV – VELECEF (0x01 0x11)

63PUBX,41 – Set Protocols and Baudrate Input message. $PUBX,41,p41x1,p41x2,p41x3,p41x4,p41x5*hh<CR><LF> Parameters Descriptions Notes

Page 120 - NAV – VELNED (0x01 0x12)

64 7.2 UBX Binary Protocol To obtain the maximum performance from GPS chips, which mainly consists of FV-25, u-blox proposed a proprietary binary pro

Page 121 - NAV – TIMEGPS (0x01 0x20)

65For the calculation of the checksum, u-blox utilizes the low-overhead checksum algorithm, which is the TCP standard (RFC 1145). The calculation of

Page 122 - NAV – TIMEUTC (0x01 0x21)

66R8 IEEE754 Double Precision 8 -1*21023 ~ 21023 ~Value*2-53 CH ASCII / ISO 8859.1 Encoding 1 Table 7.1 The types of data. 7.2.2 Classificati

Page 123 - NAV – CLOCK (0x01 0x22)

677.2.4 UBX Messages UBX Class ACK This class is used for responding a CFG message. ACK – ACK (0x05 0x01) Message acknowledged. Header ID Data Len

Page 124 - NAV – SVINFO (0x01 0x30)

68ACK – NAK (0x05 0x00) Message not-acknowledged. Header ID Data Length Data Checksum 0xB5 0x62 0x05 0x00 2 See below CK_A CK_B Data Offset byt

Page 125 - NAV – DGPS (0x01 0x31)

69UBX Class AID This class is used to support AGPS function or send aiding data, such as time, position, almanac, and ephemeris, to the GPS receiver.

Page 126 - NAV – SBAS (0x01 0x32)

7Chapter 7 Available NMEA and UBX1 Messages This chapter lists the available NMEA and u-blox proprietary (UBX) messages for the module. Chapter 8 Tro

Page 127

70AID – DATA (0x0B 0x10) It’s a request to poll all the GPS initial aiding data. This message will activate the sending of AID-INI, AID-HUI, AID-EPH,

Page 128

71AID – INI (0x0B 0x01) It’s a poll request when “data length” is equal to 0. Poll GPS initial aiding data. Header ID Data Length Data Checksum 0xB5

Page 129

72 AID – HUI (0x0B 0x02) It’s a poll request when “data length” is equal to 0. Poll GPS health, UTC, and Ionosphere data. Header ID Data Length Data

Page 130 - RXM – SVSI (0x02 0x20)

7348 R4 Alpha3 Klobuchar parameters 52 R4 Beta0 Klobuchar parameters 56 R4 Beta1 Klobuchar parameters 60 R4 Beta2 Klobuchar parameters 64 R4 Beta

Page 131

74AID – ALM (0x0B 0x30) It’s a poll request when “data length” is equal to 0. Poll all available aiding almanac data. Header ID Data Length Data Che

Page 132

7528 U4 Almanac – WORD5 32 U4 Almanac – WORD6 36 U4 Almanac – WORD7 NOTE: 1. WORD0 ~ WORD7 contain the data following the Hand-Over Word (HOW) in

Page 133

76AID – EPH (0x0B 0x31) It’s a poll request when “data length” is equal to 0. Poll all available aiding ephemeris data. Header ID Data Length Data C

Page 134

7732+n*96 U4 Sub-frame 1 – WORD6 36+n*96 U4 Sub-frame 1 – WORD7 40+n*96 U4 Sub-frame 2 – WORD0 44+n*96 U4 Sub-frame 2 – WORD1 48+n*96

Page 135 - RXM – POSREQ (0x02 0x40)

78UBX Class CFG This class is used to configure the GPS module and output the current configuration of the GPS module. The module will respond the AC

Page 136

7910 – 2 stop bit ; 11 – reserved Bit[16] 0 – LSB first bit order 1 – MSB first bit order Bit[19] 0 – 16x oversampling 1 – 8x oversampling 8+N*20 U4

Page 137 - TIM – TP (0x0D 0x01)

8 Chapter 1 Introduction In this chapter, the main goal of FV-25 will be described and then the features of the FV-25 module will be specified in or

Page 138

80CFG – MSG (0x06 0x01) It’s a poll request. Poll a message configuration. Header ID Data Length Data Checksum 0xB5 0x62 0x06 0x01 2 See below C

Page 139

81Data Offset bytes Format Descriptions Notes 0 U1 Class ID 1 U1 Message ID 2 U1 Message rate on the current target

Page 140 - Chapter 8 Troubleshooting

82CFG – NMEA (0x06 0x17) It’s a poll request. Poll the NMEA protocol configuration. Header ID Data Length Data Checksum 0xB5 0x62 0x06 0x17 0 Non

Page 141 - Table 8.1 Troubleshooting

83CFG – RATE (0x06 0x08) It’s a poll request. Poll the current navigation/measurement rate setting. The module will respond the same message defined

Page 142

84CFG – CFG (0x06 0x09) It’s a command message. The message will clear, save, and load configurations. The command consists of the three masks (clear

Page 143

85UBX-CFG-ANT) 11 Reserved 12 ~ 15 Reserved for user applications 16 ~ 31 Reserved

Page 144

86CFG – TP (0x06 0x07) It’s a poll request. Poll time pulse information. The module will respond the same message defined below (I/O message). Heade

Page 145

87CFG – NAV (0x06 0x03) It’s a poll request. Poll engine settings for navigation. The module will respond the same message defined below (I/O message

Page 146

88used in the navigation solution 6 U1 DGPS timetag rounding 1 – enable 0 – disable 7 U1 Timeout for differential correction data (s) 8 U1

Page 147

89CFG – DAT (0x06 0x06) It’s a poll request. Poll datum setting. The module will respond the same message defined below (I/O message). Header ID Dat

Page 148

9sensitivity for weak signals without sacrificing accuracy, AGPS function, DGPS function which is supported by RTCM, WAAS, and EGNOS, and flexibility

Page 149

90seconds) 40 R4 Scale change (ppm) 0.0 ~ 50.0 CFG – DAT (0x06 0x06) It’s an output message. Poll the current datum. If the datum number is –1, t

Page 150

91CFG – INF (0x06 0x02) It’s a poll request. It’s used to identify the output protocol. Header ID Data Length Data Checksum 0xB5 0x62 0x06 0x02 1

Page 151

9213 – User1-defined protocol 14 – User2-defined protocol 15 – User3-defined protocol 16 ~ 255 – reserved 1+N*8 U1 Reserved 2+N*8 U2 Reserved

Page 152

93CFG – RST (0x06 0x04) It’s an input message. It’s used to reset receiver or clear backup data structure. Header ID Data Length Data Checksum 0xB5

Page 153

94CFG – RXM (0x06 0x11) It’s a poll request. It’s used to poll RXM configuration. The module responds the same message defined below. Header ID Data

Page 154

95CFG – ANT (0x06 0x13) It’s a poll request. It’s used to poll antenna control settings. The module responds the same message defined below. Header

Page 155 - Ellipsoids

96CFG – FXN (0x06 0x0E) It’s a poll request. It’s used to poll power saving (FixNow) mode configuration. The module responds the same message defined

Page 156 - Rotation and Scale Table

97CFG – SBAS (0x06 0x16) It’s a command message. It’s used to configure SBAS systems, such as WAAS, EGNOS, and MSAS. More information about SBAS serv

Page 157 - Appendix B Acronyms

98CFG – TM (0x06 0x10) It’s a poll request. It’s used to poll time mark configuration. Header ID Data Length Data Checksum 0xB5 0x62 0x06 0x10 0

Page 158 - References

99CFG – EKF (0x06 0x12) It’s a poll request. It’s used to poll EKF configuration. The module responds the same message defined below. Header ID Data

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