--- pageClass: is-wide-page --- # TecsStatus (повідомлення UORB) **TOPICS:** tecs_status ## Fields | Назва | Тип | Unit [Frame] | Range/Enum | Опис | | ---------------------------------------------------------------------------------------------------------------- | --------- | ---------------------------------------------------------------- | ---------- | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ | | timestamp | `uint64` | | | time since system start (microseconds) | | altitude_sp | `float32` | | | Altitude setpoint AMSL [m] | | altitude_reference | `float32` | | | Altitude setpoint reference AMSL [m] | | altitude_time_constant | `float32` | | | Time constant of the altitude tracker [s] | | height_rate_reference | `float32` | | | Height rate setpoint reference [m/s] | | height_rate_direct | `float32` | | | Direct height rate setpoint from velocity reference generator [m/s] | | height_rate_setpoint | `float32` | | | Height rate setpoint [m/s] | | height_rate | `float32` | | | Height rate [m/s] | | equivalent_airspeed_sp | `float32` | | | Equivalent airspeed setpoint [m/s] | | true_airspeed_sp | `float32` | | | True airspeed setpoint [m/s] | | true_airspeed_filtered | `float32` | | | True airspeed filtered [m/s] | | true_airspeed_derivative_sp | `float32` | | | True airspeed derivative setpoint [m/s^2] | | true_airspeed_derivative | `float32` | | | True airspeed derivative [m/s^2] | | true_airspeed_derivative_raw | `float32` | | | True airspeed derivative raw [m/s^2] | | total_energy_rate_sp | `float32` | | | Total energy rate setpoint [m^2/s^3] | | total_energy_rate | `float32` | | | Total energy rate estimate [m^2/s^3] | | total_energy_balance_rate_sp | `float32` | | | Energy balance rate setpoint [m^2/s^3] | | total_energy_balance_rate | `float32` | | | Energy balance rate estimate [m^2/s^3] | | throttle_integ | `float32` | | | Throttle integrator value [-] | | pitch_integ | `float32` | | | Pitch integrator value [rad] | | throttle_sp | `float32` | | | Current throttle setpoint [-] | | pitch_sp_rad | `float32` | | | Current pitch setpoint [rad] | | throttle_trim | `float32` | | | estimated throttle value [0,1] required to fly level at equivalent_airspeed_sp in the current atmospheric conditions | | underspeed_ratio | `float32` | | | 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0. | | fast_descend_ratio | `float32` | | | value indicating if fast descend mode is enabled with ramp up and ramp down [0-1] | ## Source Message [Source file (GitHub)](https://github.com/PX4/PX4-Autopilot/blob/main/msg/TecsStatus.msg) :::details Click here to see original file ```c uint64 timestamp # time since system start (microseconds) float32 altitude_sp # Altitude setpoint AMSL [m] float32 altitude_reference # Altitude setpoint reference AMSL [m] float32 altitude_time_constant # Time constant of the altitude tracker [s] float32 height_rate_reference # Height rate setpoint reference [m/s] float32 height_rate_direct # Direct height rate setpoint from velocity reference generator [m/s] 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 float32 underspeed_ratio # 0: no underspeed, 1: maximal underspeed. Controller takes measures to avoid stall proportional to ratio if >0. float32 fast_descend_ratio # value indicating if fast descend mode is enabled with ramp up and ramp down [0-1] ``` :::