forked from Archive/PX4-Autopilot
11 lines
522 B
Plaintext
11 lines
522 B
Plaintext
uint64 timestamp # time since system start (microseconds)
|
|
|
|
# body angular rates in NED frame
|
|
float32 roll # [rad/s] roll rate setpoint
|
|
float32 pitch # [rad/s] pitch rate setpoint
|
|
float32 yaw # [rad/s] yaw rate setpoint
|
|
|
|
# For clarification: For multicopters thrust_body[0] and thrust[1] are usually 0 and thrust[2] is the negative throttle demand.
|
|
# For fixed wings thrust_x is the throttle demand and thrust_y, thrust_z will usually be zero.
|
|
float32[3] thrust_body # Normalized thrust command in body NED frame [-1,1]
|