TECS Member List

This is the complete list of members for TECS, including all inherited members.

_airspeed_enabled	TECS	private
_climbout_mode_active	TECS	private
_detect_uncommanded_descent()	TECS	private
_detect_underspeed()	TECS	private
_detect_underspeed_enabled	TECS	private
_dt	TECS	private
_EAS	TECS	private
_EAS_setpoint	TECS	private
_height_error_gain	TECS	private
_height_setpoint_gain_ff	TECS	private
_hgt_estimate_freq	TECS	private
_hgt_rate_setpoint	TECS	private
_hgt_setpoint	TECS	private
_hgt_setpoint_adj	TECS	private
_hgt_setpoint_adj_prev	TECS	private
_hgt_setpoint_in_prev	TECS	private
_hgt_setpoint_prev	TECS	private
_in_air	TECS	private
_indicated_airspeed_max	TECS	private
_indicated_airspeed_min	TECS	private
_initialize_states(float pitch, float throttle_cruise, float baro_altitude, float pitch_min_climbout, float eas_to_tas)	TECS	private
_integrator_gain	TECS	private
_last_pitch_setpoint	TECS	private
_last_throttle_setpoint	TECS	private
_load_factor_correction	TECS	private
_max_climb_rate	TECS	private
_max_sink_rate	TECS	private
_min_sink_rate	TECS	private
_pitch_damping_gain	TECS	private
_pitch_integ_state	TECS	private
_pitch_setpoint	TECS	private
_pitch_setpoint_max	TECS	private
_pitch_setpoint_min	TECS	private
_pitch_setpoint_unc	TECS	private
_pitch_speed_weight	TECS	private
_pitch_time_constant	TECS	private
_pitch_update_timestamp	TECS	private
_SEB_error	TECS	private
_SEB_rate_error	TECS	private
_SKE_estimate	TECS	private
_SKE_rate	TECS	private
_SKE_rate_setpoint	TECS	private
_SKE_setpoint	TECS	private
_SPE_estimate	TECS	private
_SPE_rate	TECS	private
_SPE_rate_setpoint	TECS	private
_SPE_setpoint	TECS	private
_speed_derivative	TECS	private
_speed_error_gain	TECS	private
_speed_update_timestamp	TECS	private
_state_update_timestamp	TECS	private
_states_initalized	TECS	private
_STE_error	TECS	private
_STE_rate_error	TECS	private
_STE_rate_max	TECS	private
_STE_rate_min	TECS	private
_tas_estimate_freq	TECS	private
_TAS_max	TECS	private
_TAS_min	TECS	private
_TAS_rate_setpoint	TECS	private
_tas_rate_state	TECS	private
_TAS_setpoint	TECS	private
_TAS_setpoint_adj	TECS	private
_TAS_setpoint_last	TECS	private
_tas_state	TECS	private
_throttle_damping_gain	TECS	private
_throttle_integ_state	TECS	private
_throttle_setpoint	TECS	private
_throttle_setpoint_max	TECS	private
_throttle_setpoint_min	TECS	private
_throttle_slewrate	TECS	private
_throttle_time_constant	TECS	private
_uncommanded_descent_recovery	TECS	private
_underspeed_detected	TECS	private
_update_energy_estimates()	TECS	private
_update_height_setpoint(float desired, float state)	TECS	private
_update_pitch_setpoint()	TECS	private
_update_speed_setpoint()	TECS	private
_update_speed_states(float airspeed_setpoint, float indicated_airspeed, float eas_to_tas)	TECS	private
_update_STE_rate_lim()	TECS	private
_update_throttle_setpoint(float throttle_cruise, const matrix::Dcmf &rotMat)	TECS	private
_vert_accel_limit	TECS	private
_vert_accel_state	TECS	private
_vert_pos_state	TECS	private
_vert_vel_state	TECS	private
airspeed_sensor_enabled()	TECS	inline
DT_DEFAULT	TECS	privatestatic
ECL_TECS_MODE enum name	TECS
ECL_TECS_MODE_BAD_DESCENT enum value	TECS
ECL_TECS_MODE_CLIMBOUT enum value	TECS
ECL_TECS_MODE_NORMAL enum value	TECS
ECL_TECS_MODE_UNDERSPEED enum value	TECS
enable_airspeed(bool enabled)	TECS	inline
get_pitch_setpoint()	TECS	inline
get_speed_weight()	TECS	inline
get_throttle_setpoint(void)	TECS	inline
handle_alt_step(float delta_alt, float altitude)	TECS	inline
hgt_rate_setpoint()	TECS	inline
hgt_setpoint_adj()	TECS	inline
operator=(const TECS &)=delete	TECS
operator=(TECS &&)=delete	TECS
pitch_integ_state()	TECS	inline
reset_state()	TECS	inline
SEB_error()	TECS	inline
SEB_rate_error()	TECS	inline
set_detect_underspeed_enabled(bool enabled)	TECS	inline
set_height_comp_filter_omega(float omega)	TECS	inline
set_heightrate_ff(float heightrate_ff)	TECS	inline
set_heightrate_p(float heightrate_p)	TECS	inline
set_indicated_airspeed_max(float airspeed)	TECS	inline
set_indicated_airspeed_min(float airspeed)	TECS	inline
set_integrator_gain(float gain)	TECS	inline
set_max_climb_rate(float climb_rate)	TECS	inline
set_max_sink_rate(float sink_rate)	TECS	inline
set_min_sink_rate(float rate)	TECS	inline
set_pitch_damping(float damping)	TECS	inline
set_roll_throttle_compensation(float compensation)	TECS	inline
set_speed_comp_filter_omega(float omega)	TECS	inline
set_speed_weight(float weight)	TECS	inline
set_speedrate_p(float speedrate_p)	TECS	inline
set_throttle_damp(float throttle_damp)	TECS	inline
set_throttle_slewrate(float slewrate)	TECS	inline
set_time_const(float time_const)	TECS	inline
set_time_const_throt(float time_const_throt)	TECS	inline
set_vertical_accel_limit(float limit)	TECS	inline
speed_derivative()	TECS	inline
STE_error()	TECS	inline
STE_rate_error()	TECS	inline
TAS_rate_setpoint()	TECS	inline
TAS_setpoint_adj()	TECS	inline
tas_state()	TECS	inline
TECS()=default	TECS
TECS(const TECS &)=delete	TECS
TECS(TECS &&)=delete	TECS
tecs_mode()	TECS	inline
throttle_integ_state()	TECS	inline
timestamp()	TECS	inline
update_pitch_throttle(const matrix::Dcmf &rotMat, float pitch, float baro_altitude, float hgt_setpoint, float EAS_setpoint, float indicated_airspeed, float eas_to_tas, bool climb_out_setpoint, float pitch_min_climbout, float throttle_min, float throttle_setpoint_max, float throttle_cruise, float pitch_limit_min, float pitch_limit_max)	TECS
update_vehicle_state_estimates(float airspeed, const matrix::Dcmf &rotMat, const matrix::Vector3f &accel_body, bool altitude_lock, bool in_air, float altitude, bool vz_valid, float vz, float az)	TECS
vert_pos_state()	TECS	inline
vert_vel_state()	TECS	inline
~TECS()=default	TECS