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GPS Receiver Board

                                GPS-24 / 24A Operating Manual

      

                    

 Rikaline

 

                                                    

Specifications subject to change without prior notice 

Rikaline

 International Corp.

     

  

14F, 171, ChengGong Rd, Sanchong CityTaipei 241, Taiwan

 

Tel: ++886 2 8973 1899  Fax: ++886 2 8973 1896   E-Mail: 

[email protected]

    Web: www.rikaline.com.tw 

17

C4.5  $PNMRX106, Datum 

This message defines the conversion model used for mapping the ECEF coordinates into the LLA ones. The 
default transformation uses WGS84 approximation. The transformation method can be changed into one 
using a reference Ellipsoid combined with a local datum, to obtain a specific estimation of the local earth 
geometry. Once the datum has been changed it will be applied to all LLA data, including the LLA navigation 
initialization Data. This message enables the receiver to be configured to use map datum from an internal 
table, or datum supplied as part of the message. 
 

Field Format 

Min 

chars

Max 

chars

Notes 

Message ID 

$PNMRX106  6 

PNMRX106 protocol header. 

Correction Mode  Unsigned 

If 1 apply EGM96 geoids correction (warning: 
should be applied only when Map Datum is equal to 
216). If 0 there is no EGM96 geoids correction. 
Reference number of the appropriate map datum to 
apply. 

Map Datum 

Int 

(0) 1 

0-218  Map datum from internal table 
500    User defined Datum 

Dx Int 

(0) 
(-)1 

(-)5 

X offset in meters (-9999 to 9999) 

Dy Int 

(0) 
(-)1 

(-)5 

Y offset in meters (-9999 to 9999) 

Dz Int 

(0) 
(-)1 

(-)5 

Z offset in meters (-9999 to 9999) 

Iflat 

Int 

(0) 1 

Inverse flatness of reference geode. The value to 
be used is (IFlat – 290) * 1000000). 
The value must be in the range [6000000, 
12000000] 

Majora 

Int 

(0) 1 

Semi major axis of reference geode. The values to 
be used is (MajorA – 6370000) * 1000). 
The value must be in the range [6000000, 
9000000] 

Checksum 

*xx 

(0) 3 

2 digits. 

Message 
terminator 

<CR> <LF> 

ASCII 13, ASCII 10. 

 

Examples: 

$PNMRX106, 0,500, -2000,-2000,-2000, 8257224, 8137000*00*xx:

  User defined Datum 

$PNMRX106, 1, 216,*xx:

   

 

 

 

 

     WGS 84 Datum 

 

C.6  $PNMRX107, Messages rate control 

This message is sent to set the automatic update rate, and to configure which messages will be 
automatically output, it is also sent from the node to report which messages are currently configured for 
automatic transmission. The $PNMRX107 message format is shown below. This message can be used to 
enable and disable multiple messages by including up to 4 message codes and associated fields in each 
$PNMRX107 message. 
The message length is limited to 80 characters, in the event that the message length would exceed 80 
characters it is divided into 2 messages. This message is supported also in a variable length format, where 
only the necessary fields are used. 
 

Field Format 

Min 

chars

Max 

chars

Notes 

Message ID  $PNMRX107  8 

PNMRX107 protocol header. 
Determines which message is being configured. 

Message 
code 

Char 3 

300 PNMRX300 

Almanac Data 

301 PNMRX301 Ephemeris Data 
302  PNMRX302 lonospheric corrections 
303 PNMRX303 UTC Time 
304  PNMRX304 GPS constellation health 
ALL  Applies to all messages 

Summary of Contents for GPS-24

Page 1: ...Rikaline International Corp 14F 171 ChengGong Rd Sanchong City Taipei 241 Taiwan R O C Phone 886 2 8973 1899 Fax 886 2 8973 1896 E Mail info rikaline com tw Web www rikaline com tw All Right Reserved...

Page 2: ...es satellite signals in 100 ms and updates position data every second 1 2 Features The GPS 24 24A provides a host of features that make it easy for integration and use 1 Position accuracy in 7m CEP 90...

Page 3: ...Differential GPS Position 1 m typical Velocity 0 05 meters second typical 5 Dynamic Conditions Altitude 10 000 meters 32 800 feet max Velocity Horisontal 300 Km Hr Vertical 36 Km Hr Acceleration 2 G m...

Page 4: ...cquisition performance If significant inaccuracy exists in the initial data or the orbital data is obsolete it may take more time to achieve a navigation solution The FirstGPS architecture provides su...

Page 5: ...tw 5 3 Hardware interface 3 1 Physical Characters 1 Size 25 9 W x 25 9 D x 2 7 H mm 2 Weight 25 g 1 02 W x 1 02 D x 0 11 H 3 1 1 Details Drawing 3 1 1 1GPS 24 to be equipped with active antenna only...

Page 6: ...ct D2 DSUEN I DSU enable D3 DSUBRE I DSU break enable D4 DSUTX O DSU transmitter D5 DSURX I DSU receiver D6 DSUACT O DSU active 3 3 Operating Modes 3 3 1 GPIO 1 4 It design as spare I O You may leave...

Page 7: ...Fax 886 2 8973 1896 E Mail info rikaline com tw Web www rikaline com tw 7 Table 3 3 Backup Battery Conditions Parameter Symbol Min Typ Max Units RTC Battery Power BAT 1 2 1 8 2 V Supply Current 10 A T...

Page 8: ...n parameters for NMEA output are 9600 baud 8 data bits stop bit and no parity Table 4 1 NMEA 0183 Output Messages NMEA Record Description GPGGA Global positioning system fixed data GPGLL Geographic po...

Page 9: ...ptions 5 1 1 GPS Receiver Module GPS 24 Standard with TTL level GPS 24 A Standard with TTL level and available to attach patch antenna on top of the board 5 2 Accessories A 10302 M Active Antenna 2M M...

Page 10: ...GA Global positioning system fixed data GPGLL Geographic position latitude longitude GPGSA GNSS DOP and active satellites GPGSV GNSS satellites in view GPRMC Recommended minimum specific GNSS data GPV...

Page 11: ...le GPGSA A 3 07 02 26 27 09 04 15 1 8 1 0 1 5 33 Table A 5 GSA Data Format Name Example Units Description Message ID GPGSA GSA protocol header Mode 1 A See Table 5 6 Mode 2 3 See Table 5 7 Satellite U...

Page 12: ...ed Minimum Specific GNSS Data RMC Table A 9 contains the values for the following example GPRMC 161229 487 A 3723 2475 N 12158 3416 W 0 13 309 62 120598 10 Table A 9 RMC Data Format Name Example Units...

Page 13: ...om tw 13 A 1 7 Time Date ZDA Table A 11 contains the values for the following example GPVTG 114523 62 12 04 2001 10 34 6E Table A 11 ZDA Data Format Name Example Units Description Message ID GPZDA ZDA...

Page 14: ...Specifications subject to change without prior notice Rikaline International Corp 14F 171 ChengGong Rd Sanchong CityTaipei 241 Taiwan Tel 886 2 8973 1899 Fax 886 2 8973 1896 E Mail info rikaline com t...

Page 15: ...ent to initialize navigation parameters to speed up initial acquisition time The PNMRX101 message format is shown below Field Format Min chars Max chars Notes Message ID PNMRX101 6 8 PNMRX101 protocol...

Page 16: ...GA every 1s and ZDA is skipped PNMRX103 GSV 2 GGA 1 ZDA 0 xx same as above but using a fixed length message PNMRX103 ALL 2 xx all messages are output every 2s PNMRX103 ALL 0 xx skips all messages C 4...

Page 17: ...9999 Dz Int 0 1 5 Z offset in meters 9999 to 9999 Iflat Int 0 1 8 Inverse flatness of reference geode The value to be used is IFlat 290 1000000 The value must be in the range 6000000 12000000 Majora I...

Page 18: ...otocol header Mask ID Int 3 3 Mask identifier possibilities are GGA GLL GSA GSV RMC VTG ZDA Mask ID Int 3 3 Mask Identifier Checksum xx 0 3 3 2 digits Message terminator CR LF 2 2 ASCII 13 ASCII 10 Ex...

Page 19: ...e executed after the reset If the last bit field is set to 1 then the actions are repeated permanently at each reset until this bit is cleared Field Format Min chars Max chars Notes Message ID PNMRX11...

Page 20: ...ties C 10 PNMRX300 Almanac Data Transfer This message format is used to transfer the almanac data between nodes it uses a packed hexadecimal format to transfer almanac data for each of the available S...

Page 21: ...these can be sent in any order provided that the 3 messages for any individual satellite are grouped together each message is individually interpreted and after a group of 3 valid messages for an SV t...

Page 22: ...ger Checksum xx 0 3 2 digits Message terminator CR LF 2 ASCII 13 ASCII 10 C 12 PNMRX302 Ionospheric correction Field Format width scale units Notes Message ID PNMRX302 8 PNMRX301 protocol header Satel...

Page 23: ...ield Format Min chars Max chars Notes Message ID PNMRX603 8 8 PNMRX603 protocol header Message Nb Int 1 1 0 Message Sequence 7 times 7xInt 1 1 Message Sequence Message Delay 7 times 7xInt 1 1 Message...

Page 24: ...CII 10 PNMRX603 message 3 Field Format Min chars Max chars Notes Message ID PNMRX603 8 8 PNMRX603 protocol header Message Nb Int 1 1 3 Acq threshold 1 Int 3 8 Acq threshold 2 Int 3 8 Noise floor Int 3...

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