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FW Position Control: add airspeed offset based on wind in Eco mode
setpoint = FW_AIRSPD_MIN + FW_LND_AIRSPD_SC * wind Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
@@ -364,6 +364,19 @@ FixedwingPositionControl::get_cruise_airspeed_setpoint(const hrt_abstime &now, c
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if (_speed_mode_current == FW_SPEED_MODE::FW_SPEED_MODE_ECO) {
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airspeed_setpoint = _param_fw_airspd_min.get();
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// Adapt cruise airspeed setpoint based on wind estimate (disable in airspeed-less mode)
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if (_airspeed_valid && _param_fw_wind_arsp_sc.get() > FLT_EPSILON) {
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wind_s wind_estimate;
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if (_wind_sub.update(&wind_estimate)) {
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const matrix::Vector2f wind(wind_estimate.windspeed_north, wind_estimate.windspeed_east);
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if (PX4_ISFINITE(wind.length())) {
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airspeed_setpoint += _param_fw_wind_arsp_sc.get() * wind.length();
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}
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}
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}
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} else if (_speed_mode_current == FW_SPEED_MODE::FW_SPEED_MODE_DASH) {
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airspeed_setpoint = _param_fw_airspd_max.get();
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}
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@@ -504,47 +517,6 @@ FixedwingPositionControl::resetAutoSpeedAdaptions()
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_speed_mode_current = FW_SPEED_MODE::FW_SPEED_MODE_NORMAL;
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}
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void
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FixedwingPositionControl::update_wind_mode()
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{
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/* If the corresponding wind threshold values are set, the wind state will change if these values are
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* passed for a certain amount of time. The wind state is then used to increase airspeed (high wind),
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* resp. decrease (low wind). It takes longer to move to a lower wind state than to a higher,
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* as in general higher airspeed is safer. */
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wind_s wind_estimate;
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if (_wind_sub.update(&wind_estimate)) {
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const matrix::Vector2f wind(wind_estimate.windspeed_north, wind_estimate.windspeed_east);
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FW_WIND_MODE fw_wind_mode_detected(FW_WIND_MODE_NORMAL);
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if (_param_fw_wind_thld_h.get() > FLT_EPSILON && wind.length() > _param_fw_wind_thld_h.get()) {
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fw_wind_mode_detected = FW_WIND_MODE_HIGH;
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} else if (_param_fw_wind_thld_l.get() > FLT_EPSILON && wind.length() < _param_fw_wind_thld_l.get()) {
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fw_wind_mode_detected = FW_WIND_MODE_LOW;
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}
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if (fw_wind_mode_detected != _fw_wind_mode_detected_prev) {
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_first_time_current_mode_detected = hrt_absolute_time();
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}
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const float min_time_detection_mode_down = 60.0f; // min time to switch to lower wind state
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const float time_since_new_mode_detected = hrt_elapsed_time(&_first_time_current_mode_detected) * 1e-6f;
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// immediately switch to higher wind mode after detection, but require minimum time within lower wind to switch to lower mode
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if (fw_wind_mode_detected > _fw_wind_mode_current) {
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_fw_wind_mode_current = fw_wind_mode_detected;
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} else if (fw_wind_mode_detected < _fw_wind_mode_current
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&& time_since_new_mode_detected > min_time_detection_mode_down) {
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_fw_wind_mode_current = fw_wind_mode_detected;
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}
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_fw_wind_mode_detected_prev = fw_wind_mode_detected;
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}
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}
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void
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FixedwingPositionControl::status_publish()
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{
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@@ -816,7 +788,6 @@ FixedwingPositionControl::control_auto(const hrt_abstime &now, const Vector2d &c
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check_eco_dash_allowed();
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updateSpeedMode();
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update_wind_mode();
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/* restore TECS parameters, in case changed intermittently (e.g. in landing handling) */
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_tecs.set_speed_weight(_param_fw_t_spdweight.get());
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@@ -285,17 +285,6 @@ private:
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bool _conditions_for_eco_dash_met{false};
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hrt_abstime _time_conditions_not_met{0};
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// wind state
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hrt_abstime _first_time_current_mode_detected{0}; ///< last time in normal wind mode
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enum FW_WIND_MODE {
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FW_WIND_MODE_LOW,
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FW_WIND_MODE_NORMAL,
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FW_WIND_MODE_HIGH,
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} _fw_wind_mode_current{FW_WIND_MODE_NORMAL}; ///< used to make wind-based airspeed setpoint adaptions
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FW_WIND_MODE _fw_wind_mode_detected_prev{FW_WIND_MODE_NORMAL};
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float _last_airspeed_setpoint{NAN};
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param_t _param_handle_airspeed_trans{PARAM_INVALID};
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@@ -477,9 +466,7 @@ private:
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(ParamFloat<px4::params::FW_TKO_PITCH_MIN>) _takeoff_pitch_min,
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//Speed mode params
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(ParamFloat<px4::params::FW_WIND_THLD_H>) _param_fw_wind_thld_h,
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(ParamFloat<px4::params::FW_WIND_THLD_L>) _param_fw_wind_thld_l,
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(ParamFloat<px4::params::FW_WIND_ARSP_OF>) _param_fw_wind_arsp_of,
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(ParamFloat<px4::params::FW_WIND_ARSP_SC>) _param_fw_wind_arsp_sc,
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(ParamInt<px4::params::FW_SPD_MODE_SET>) _fw_spd_mode_set,
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(ParamFloat<px4::params::FW_ALT_MIN>) fw_alt_min,
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@@ -856,54 +856,22 @@ PARAM_DEFINE_INT32(FW_GPSF_LT, 30);
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PARAM_DEFINE_FLOAT(FW_GPSF_R, 15.0f);
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/**
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* High wind threshold
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* Wind-based airspeed scaling factor in Eco
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*
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* If the current wind estimate is above this threshold,the value of FW_WIND_ARSP_OF
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* is added to the cruise airspeed setpoint.
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* Set to zero number to disable wind-based airspeed setpoint up-scaling.
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* Multiplying this factor with the current absolute wind estimate gives the airspeed offset
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* added to the setpoint (which is FW_AIRSPD_MIN) in Eco mode. This helps to make the
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* system more robust against disturbances in high wind.
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*
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* @unit m/s
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* @min 0.0
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* @max 30
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* @decimal 1
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* @increment 0.5
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* @group FW TECS
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*/
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PARAM_DEFINE_FLOAT(FW_WIND_THLD_H, 0.0f);
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/**
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* Low wind threshold
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* setpoint = FW_AIRSPD_MIN + FW_LND_AIRSPD_SC * wind
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*
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* If the current wind estimate is below this threshold for 60 seconds,the value of
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* FW_WIND_ARSP_OF is subtracted from the cruise airspeed setpoint.
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* Set to zero to disable wind-based airspeed setpoint down-scaling.
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*
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* @unit m/s
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* @unit norm
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* @min 0
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* @max 30
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* @decimal 1
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* @increment 0.5
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* @group FW TECS
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*/
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PARAM_DEFINE_FLOAT(FW_WIND_THLD_L, 0.0f);
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/**
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* Wind-based airspeed setpoint offset
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*
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* Airspeed setpoint offset that is added/subtracted to the cruise airspeed setpoint if wind-based setpoint
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* adaption is enabled for either or both high and low winds (FW_WIND_THLD_H and FW_WIND_THLD_L).
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* If in high wind condition, this offset is added to the cruise airspeed setpoint.
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* If in low wind condition, this offset is subtracted from the cruise airspeed setpoint.
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* Note: manual airspeed setpoints via sticks must be disabled for wind-based adaption to work (see FW_POS_STK_CONF).
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*
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* @unit m/s
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* @min 0
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* @max 10
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* @decimal 1
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* @max 2
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* @decimal 2
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* @increment 0.01
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* @group FW TECS
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*/
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PARAM_DEFINE_FLOAT(FW_WIND_ARSP_OF, 1.0f);
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PARAM_DEFINE_FLOAT(FW_WIND_ARSP_SC, 0.0f);
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/**
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* FW Speed mode setting
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