3DM
®
-GX5-35
DCP Manual
5.1.9
CF Euler Angles (0x80, 0x0C)
Description
Pitch, Roll, and Yaw (aircraft) values.
This value is produced by the Complementary Filter fusion algorithm.
Notes
This is a three component vector containing the Roll, Pitch and Yaw angles in radi-
ans. It is computed by the IMU/AHRS from the orientation matrix
M.
Field Format
Field
Length
Data
Descriptor
Message Data
14 (0x0E)
0x0C
Binary
Offset
Description
Data
Type
Units
0
Roll
Float
Radians
4
Pitch
Float
Radians
8
Yaw
Float
Radians
76