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synced 2026-10-03 07:28:54 +08:00
Support gliding setpoints for autonomous soaring (#14643)
* Enable offboard gliding position setpoints Adds a capability to make the vehicle glide when given position setpoints. Gliding setpoints are enabled by setting POSITION_TARGET_TYPEMASK_Z_IGNORE, POSITION_TARGET_TYPEMASK_VZ_IGNORE, POSITION_TARGET_TYPEMASK_AZ_IGNORE on the typemask of position setpoints. Include zero cruising throttle Invalid setpoints with nan * Handle nans for curise_throttle
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@@ -668,8 +668,7 @@ FixedwingPositionControl::control_position(const hrt_abstime &now, const Vector2
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float mission_throttle = _param_fw_thr_cruise.get();
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if (PX4_ISFINITE(pos_sp_curr.cruising_throttle) &&
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pos_sp_curr.cruising_throttle > 0.01f) {
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pos_sp_curr.cruising_throttle >= 0.0f) {
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mission_throttle = pos_sp_curr.cruising_throttle;
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}
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@@ -684,16 +683,34 @@ FixedwingPositionControl::control_position(const hrt_abstime &now, const Vector2
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_att_sp.roll_body = _l1_control.get_roll_setpoint();
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_att_sp.yaw_body = _l1_control.nav_bearing();
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float tecs_fw_thr_min;
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float tecs_fw_thr_max;
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float tecs_fw_mission_throttle;
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if (mission_throttle < _param_fw_thr_min.get()) {
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/* enable gliding with this waypoint */
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_tecs.set_speed_weight(2.0f);
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tecs_fw_thr_min = 0.0;
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tecs_fw_thr_max = 0.0;
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tecs_fw_mission_throttle = 0.0;
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} else {
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tecs_fw_thr_min = _param_fw_thr_min.get();
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tecs_fw_thr_max = _param_fw_thr_max.get();
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tecs_fw_mission_throttle = mission_throttle;
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}
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tecs_update_pitch_throttle(now, pos_sp_curr.alt,
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calculate_target_airspeed(mission_airspeed, ground_speed),
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radians(_param_fw_p_lim_min.get()) - radians(_param_fw_psp_off.get()),
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radians(_param_fw_p_lim_max.get()) - radians(_param_fw_psp_off.get()),
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_param_fw_thr_min.get(),
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_param_fw_thr_max.get(),
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mission_throttle,
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tecs_fw_thr_min,
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tecs_fw_thr_max,
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tecs_fw_mission_throttle,
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false,
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radians(_param_fw_p_lim_min.get()));
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} else if (pos_sp_curr.type == position_setpoint_s::SETPOINT_TYPE_LOITER) {
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/* waypoint is a loiter waypoint */
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@@ -741,13 +758,31 @@ FixedwingPositionControl::control_position(const hrt_abstime &now, const Vector2
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_tecs.set_time_const_throt(_param_fw_thrtc_sc.get() * _param_fw_t_thro_const.get());
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}
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float tecs_fw_thr_min;
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float tecs_fw_thr_max;
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float tecs_fw_mission_throttle;
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if (mission_throttle < _param_fw_thr_min.get()) {
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/* enable gliding with this waypoint */
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_tecs.set_speed_weight(2.0f);
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tecs_fw_thr_min = 0.0;
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tecs_fw_thr_max = 0.0;
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tecs_fw_mission_throttle = 0.0;
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} else {
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tecs_fw_thr_min = _param_fw_thr_min.get();
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tecs_fw_thr_max = _param_fw_thr_max.get();
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tecs_fw_mission_throttle = _param_fw_thr_cruise.get();
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}
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tecs_update_pitch_throttle(now, alt_sp,
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calculate_target_airspeed(mission_airspeed, ground_speed),
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radians(_param_fw_p_lim_min.get()) - radians(_param_fw_psp_off.get()),
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radians(_param_fw_p_lim_max.get()) - radians(_param_fw_psp_off.get()),
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_param_fw_thr_min.get(),
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_param_fw_thr_max.get(),
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_param_fw_thr_cruise.get(),
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tecs_fw_thr_min,
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tecs_fw_thr_max,
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tecs_fw_mission_throttle,
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false,
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radians(_param_fw_p_lim_min.get()));
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@@ -811,6 +811,10 @@ MavlinkReceiver::handle_message_set_position_target_local_ned(mavlink_message_t
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bool is_land_sp = (bool)(set_position_target_local_ned.type_mask & 0x2000);
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bool is_loiter_sp = (bool)(set_position_target_local_ned.type_mask & 0x3000);
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bool is_idle_sp = (bool)(set_position_target_local_ned.type_mask & 0x4000);
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bool is_gliding_sp = (bool)(set_position_target_local_ned.type_mask &
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(POSITION_TARGET_TYPEMASK::POSITION_TARGET_TYPEMASK_Z_IGNORE
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| POSITION_TARGET_TYPEMASK::POSITION_TARGET_TYPEMASK_VZ_IGNORE
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| POSITION_TARGET_TYPEMASK::POSITION_TARGET_TYPEMASK_AZ_IGNORE));
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offboard_control_mode.timestamp = hrt_absolute_time();
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_offboard_control_mode_pub.publish(offboard_control_mode);
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@@ -851,6 +855,9 @@ MavlinkReceiver::handle_message_set_position_target_local_ned(mavlink_message_t
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} else if (is_idle_sp) {
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pos_sp_triplet.current.type = position_setpoint_s::SETPOINT_TYPE_IDLE;
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} else if (is_gliding_sp) {
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pos_sp_triplet.current.cruising_throttle = 0.0f;
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} else {
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pos_sp_triplet.current.type = position_setpoint_s::SETPOINT_TYPE_POSITION;
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}
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@@ -1912,6 +1912,7 @@ bool Mission::position_setpoint_equal(const position_setpoint_s *p1, const posit
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(p1->acceleration_is_force == p2->acceleration_is_force) &&
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(fabsf(p1->acceptance_radius - p2->acceptance_radius) < FLT_EPSILON) &&
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(fabsf(p1->cruising_speed - p2->cruising_speed) < FLT_EPSILON) &&
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(fabsf(p1->cruising_throttle - p2->cruising_throttle) < FLT_EPSILON));
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((fabsf(p1->cruising_throttle - p2->cruising_throttle) < FLT_EPSILON) || (!PX4_ISFINITE(p1->cruising_throttle)
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&& !PX4_ISFINITE(p2->cruising_throttle))));
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}
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@@ -240,7 +240,7 @@ public:
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/**
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* Set the target throttle
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*/
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void set_cruising_throttle(float throttle = -1.0f) { _mission_throttle = throttle; }
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void set_cruising_throttle(float throttle = NAN) { _mission_throttle = throttle; }
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/**
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* Get the acceptance radius given the mission item preset radius
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@@ -393,7 +393,7 @@ private:
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float _mission_cruising_speed_mc{-1.0f};
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float _mission_cruising_speed_fw{-1.0f};
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float _mission_throttle{-1.0f};
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float _mission_throttle{NAN};
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// update subscriptions
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void params_update();
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@@ -907,7 +907,7 @@ Navigator::get_cruising_throttle()
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return _mission_throttle;
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} else {
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return -1.0f;
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return NAN;
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}
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}
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