SYNCRELINSPVACMP

Compressed Synchronous Relative INSPVA log

Platform: 

OEM719, OEM729, OEM7500, OEM7600, OEM7700, OEM7720, PwrPak7, CPT7, CPT7700, SMART7-S

This log contains the SYNCRELINSPVA log information compressed into a NMEA 2000 fast packet message for CAN output. The information in the following table is the data portion of the SYNCRELINSPVACMP NMEA 2000 message. Refer to the National Marine Electronics Association (NMEA) NMEA2000(r) Standard rev 2.0 - January/2013 document for full details on this message output and the NMEA 2000 fast packet protocol.

The PGN of this message is configured using the PGNCONFIG command.

The computed Position, Velocity and Attitude (PVA) delta information is valid once the rover and base SPAN solutions have both reached Alignment Complete (rover INSStatus and base INSStatus are both INS_ALIGNMENT_COMPLETE, INS_SOLUTION_GOOD, INS_SOLUTION_FREE or INS_HIGH_VARIANCE). The relative PVA quality depends on the absolute INS solution quality of both the base and rover, the GNSS relative position (ALIGN) quality, latency of corrections messages from base to rover (differential age) and rate of dynamics change of each unit but not on the absolute position solution accuracy of either base or rover.

To use the SYNCRELINSPVACMP log, the receiver requires a Relative INS capable model.

Message ID: 2538

Log Type: Synch

Rate Restriction: SYNC[200Hz]

Recommended Input:

LOG CCOM1 SYNCRELINSPVACMP ONTIME 1

Field

Field Type

Description

Quantization

Range

Binary Format

ASCII Convert String

Scale Factor

1

Message Time

Time from the beginning of the GPS week (s)

1 ms

0 – 604799.999 seconds

Ulong

0.001

2

DeltaPosX

Difference in the position between the two receivers (m).

The position difference is relative to the output frame:

BODY = along the X-axis

ECEF = along the X-axis

Local level = Northing

0.1 mm

±214 km

Long

%1d

0.0001

3

DeltaPosY

Difference in the position between the two receivers (m).

The position difference is relative to the output frame:

BODY = along the Y-axis

ECEF = along the Y-axis

Local level = Easting

0.1 mm

±214 km

Long

%1d

0.0001

4

DeltaPosZ

Difference in the position between the two receivers (m).

The position difference is relative to the output frame:

BODY = along the Z-axis

ECEF = along the Z-axis

Local level = Up

0.1 mm

±214 km

Long

%1d

0.0001

5

DeltaVelX

Difference in velocity between the two receivers (m/s).

The position difference is relative to the output frame:

BODY = along the X-axis

ECEF = along the X-axis

Local level = Northing

0.002 m/s

±262 m/s

18 bit signed integer

%ld

0.002

6

DeltaVelY

Difference in velocity between the two receivers (m/s).

The position difference is relative to the output frame:

BODY = along the Y-axis

ECEF = along the Y-axis

Local level = Easting

0.002 m/s

±262 m/s

18 bit signed integer

%ld

0.002

7

DeltaVelZ

Difference in velocity between the two receivers (m/s).

The position difference is relative to the output frame:

BODY = along the Z-axis

ECEF = along the Z-axis

Local level = Up

0.002 m/s

±262 m/s

18 bit signed integer

%ld

0.002

8

DeltaRoll

Difference in roll between the two receivers (degrees).

Right-handed rotation around Y axis.

0.01 degrees

±180 degrees

Short

%hd

0.01

9

DeltaPitch

Difference in pitch between the two receivers (degrees).

Right-handed rotation around X axis.

0.01 degrees

±180 degrees

Short

%hd

0.01

10

DeltaHeading

Difference in heading (azimuth) between the two receivers (degrees).

Left-handed rotation around Z axis.

0.01 degrees

±180 degrees

Short

%hd

0.01

11

Diff Age

Differential age in seconds.

(256 is 25.6 sconds or greater)

0.1 seconds

0 – 25.6 seconds

Uchar

%hhd

0.1

12

Rover ID

Rover receiver ID string, up to 4 ASCII characters in character order, pad with zeroes.

Char[4]

13

Rover INSStatus

INS status of the rover receiver.

See Table: Inertial Solution Status

5 bit Enum

14

Base ID

Base receiver ID string.

Char[4]

15

Base INSStatus

INS status of the base receiver.

See Table: Inertial Solution Status

5 bit Enum

16

RTK Status

Status of the current RTK vector between the base and rover.

See Table: Position or Velocity Type

8 bit Enum

17

ExtStatus

Extended solution status.

See Table: Relative INS Extended Solution Status

12 bit Hex

%03hx

18

Output Frame

The current output frame as specified using the SETRELINSOUTPUTFRAME command

See SETRELINSOUTPUTFRAME command

4 bit Enum