3DM-GX5-45
™
GNSS-Aided Inertial Navigation System
DCP Manual
5.3.9
Orientation, Euler Angles (0x82, 0x05)
Description
Estimated Pitch, Roll, and Yaw (aircraft) values.
Notes
This is a three component vector containing the Roll, Pitch and Yaw angles in
radians. It is computed by the INS from the orientation quaternion
Q.
Valid Flag Mapping:
0x0000 – Euler Angles are Invalid
0x0001 – Euler Angles Valid
Field Format
Field
Length
Data
Descriptor
Message Data
16 (0x10)
0x05
Binary
Offset
Description
Data
Type
Units
0
Roll
Float
Radians
4
Pitch
Float
Radians
8
Yaw
Float
Radians
12
Valid Flags
U16
See Notes
159