|
float | q1 |
| True attitude quaternion component 1, w (1 in null-rotation)
|
|
float | q2 |
| True attitude quaternion component 2, x (0 in null-rotation)
|
|
float | q3 |
| True attitude quaternion component 3, y (0 in null-rotation)
|
|
float | q4 |
| True attitude quaternion component 4, z (0 in null-rotation)
|
|
float | roll |
| Attitude roll expressed as Euler angles, not recommended except for human-readable outputs.
|
|
float | pitch |
| Attitude pitch expressed as Euler angles, not recommended except for human-readable outputs.
|
|
float | yaw |
| Attitude yaw expressed as Euler angles, not recommended except for human-readable outputs.
|
|
float | xacc |
| X acceleration m/s/s.
|
|
float | yacc |
| Y acceleration m/s/s.
|
|
float | zacc |
| Z acceleration m/s/s.
|
|
float | xgyro |
| Angular speed around X axis rad/s.
|
|
float | ygyro |
| Angular speed around Y axis rad/s.
|
|
float | zgyro |
| Angular speed around Z axis rad/s.
|
|
float | lat |
| Latitude in degrees.
|
|
float | lon |
| Longitude in degrees.
|
|
float | alt |
| Altitude in meters.
|
|
float | std_dev_horz |
| Horizontal position standard deviation.
|
|
float | std_dev_vert |
| Vertical position standard deviation.
|
|
float | vn |
| True velocity in m/s in NORTH direction in earth-fixed NED frame.
|
|
float | ve |
| True velocity in m/s in EAST direction in earth-fixed NED frame.
|
|
float | vd |
| True velocity in m/s in DOWN direction in earth-fixed NED frame.
|
|
The documentation for this struct was generated from the following file: