mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-04-14 10:07:39 +08:00
36 lines
1.5 KiB
Plaintext
36 lines
1.5 KiB
Plaintext
uint64 timestamp # time since system start (microseconds)
|
|
|
|
float32 altitude_sp # Altitude setpoint AMSL [m]
|
|
float32 altitude_sp_filtered # Altitude setpoint filtered AMSL [m]
|
|
float32 height_rate_setpoint # Height rate setpoint [m/s]
|
|
float32 height_rate # Height rate [m/s]
|
|
float32 equivalent_airspeed_sp # Equivalent airspeed setpoint [m/s]
|
|
float32 true_airspeed_sp # True airspeed setpoint [m/s]
|
|
float32 true_airspeed_filtered # True airspeed filtered [m/s]
|
|
float32 true_airspeed_derivative_sp # True airspeed derivative setpoint [m/s^2]
|
|
float32 true_airspeed_derivative # True airspeed derivative [m/s^2]
|
|
float32 true_airspeed_derivative_raw # True airspeed derivative raw [m/s^2]
|
|
|
|
float32 total_energy_rate_sp # Total energy rate setpoint [m^2/s^3]
|
|
float32 total_energy_rate # Total energy rate estimate [m^2/s^3]
|
|
|
|
float32 total_energy_balance_rate_sp # Energy balance rate setpoint [m^2/s^3]
|
|
float32 total_energy_balance_rate # Energy balance rate estimate [m^2/s^3]
|
|
|
|
float32 throttle_integ # Throttle integrator value [-]
|
|
float32 pitch_integ # Pitch integrator value [rad]
|
|
|
|
float32 throttle_sp # Current throttle setpoint [-]
|
|
float32 pitch_sp_rad # Current pitch setpoint [rad]
|
|
float32 throttle_trim # estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions
|
|
|
|
# TECS mode
|
|
uint8 mode
|
|
uint8 TECS_MODE_NORMAL = 0
|
|
uint8 TECS_MODE_UNDERSPEED = 1
|
|
uint8 TECS_MODE_TAKEOFF = 2
|
|
uint8 TECS_MODE_LAND = 3
|
|
uint8 TECS_MODE_LAND_THROTTLELIM = 4
|
|
uint8 TECS_MODE_BAD_DESCENT = 5
|
|
uint8 TECS_MODE_CLIMBOUT = 6
|