NMEA-0183 message: PTNL,REX
Rover Extended output
The PTNL,REX message is only populated when a receiver has MBCMR or MBCMRx correction inputs and can perform a Moving Base vector solution. This Rover Extended output provides the rover position derived from the moving base corrections, the constellations and number of satellites used, and the vector components (East, North, Up) from the source of the corrections to the rover antenna.
To produce REX output, the following are needed:
-
Valid primary fix
-
External vector from Moving Base CMR/CMR+/CMRx input
-
Valid reference time stamp
-
Valid reference ID (>= 0)
-
Valid reference accuracy figure-of-merit, including "0" (i.e., "unknown" or "N/A")
An example of the PTNL,REX message string is:
$PTNL,REX,170818.00,GREB,27,3723.09414105,N,12200.32556922,W,-6.260,0.029,0.029,0.029,
0.000,0.000,0.001,0.002,0.003,0.005,20,3*48
PTNL,REX message fields
Field |
Meaning |
---|---|
0 |
TalkerID $PTNL |
1 |
Message ID REX |
2 |
UTC time of position fix, in hhmmss.ss format. Hours must be two numbers, so may be padded. For example, 7 is shown as 07. In this example: 170818.00 |
3 |
Constellations used in solution G = GPS, R = GLONASS, E = Galileo, B = Beidou, Z = QZSS, I = NavIC A GPS and GLONASS result is reported as "GR". In this example: GREB. |
4 |
Number of satellites being used in the position In this example: 27 |
5 |
Latitude of rover in degrees and decimal minutes (ddmm.mmmmmm) In this example: 37°23.09414105' |
6 |
Direction of latitude: N: North In this example: N |
7 |
Longitude of rover vector position, in degrees and decimal minutes (dddmm.mmmmmmmm). Should contain three digits of ddd. In this example: 122°00.32556922' |
8 |
Direction of longitude: E: East In this example: W |
9 |
Height, [h].hhh, of the rover vector antenna, in meters, above WGS-84 ellipsoid. In this example: -6.260 |
10 |
Longitude, [x].xxx, 1-sigma error (N/S), absolute, in meters 1 In this example: 0.029 |
11 |
Latitude [x].xxx, 1-sigma error (E/W), absolute, in meters 1 In this example: 0.029 |
12 |
Altitude [x].xxx, 1-sigma error, absolute, in meters 1 In this example: 0.029 |
13 |
Vector East [x].xxx +E, in meters In this example: 0.000 |
14 |
Vector North [x].xxx +N, in meters In this example: 0.000 |
15 |
Vector Up [x].xxx +U, in meters In this example: 0.001 |
16 |
Vector East component 1-sigma error, in meters In this example: 0.002 |
17 |
Vector North component 1-sigma error, in meters In this example: 0.003 |
18 |
Vector Up component 1-sigma error, in meters In this example: 0.005 |
19 |
Reference Station ID [r] In this example: 20 |
20 |
Vector Fix Quality Indicator: 0: Fix not available or invalid |
21 |
The checksum data, always begins with * In this example: *48 |
1. The accuracy estimate reflects the uncertainty of the rover absolute position. This is based on both the accuracy of base and the accuracy of the vector.