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Add fw pos control states
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@ -867,57 +867,6 @@ FixedwingPositionControl::move_position_setpoint_for_vtol_transition(position_se
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}
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}
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void
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FixedwingPositionControl::control_auto(const float control_interval, const Vector2d &curr_pos,
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const Vector2f &ground_speed, const position_setpoint_s &pos_sp_prev, const position_setpoint_s &pos_sp_curr,
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const position_setpoint_s &pos_sp_next)
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{
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position_setpoint_s current_sp = pos_sp_curr;
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move_position_setpoint_for_vtol_transition(current_sp);
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const uint8_t position_sp_type = handle_setpoint_type(current_sp);
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_position_sp_type = position_sp_type;
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if (position_sp_type == position_setpoint_s::SETPOINT_TYPE_LOITER
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|| current_sp.type == position_setpoint_s::SETPOINT_TYPE_LOITER) {
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publishOrbitStatus(current_sp);
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}
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switch (position_sp_type) {
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case position_setpoint_s::SETPOINT_TYPE_IDLE:
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_att_sp.thrust_body[0] = 0.0f;
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_att_sp.roll_body = 0.0f;
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_att_sp.pitch_body = radians(_param_fw_psp_off.get());
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break;
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case position_setpoint_s::SETPOINT_TYPE_POSITION:
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control_auto_position(control_interval, curr_pos, ground_speed, pos_sp_prev, current_sp);
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break;
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case position_setpoint_s::SETPOINT_TYPE_LOITER:
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control_auto_loiter(control_interval, curr_pos, ground_speed, pos_sp_prev, current_sp, pos_sp_next);
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break;
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}
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/* Copy thrust output for publication, handle special cases */
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if (position_sp_type == position_setpoint_s::SETPOINT_TYPE_IDLE) {
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_att_sp.thrust_body[0] = 0.0f;
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} else {
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// when we are landed state we want the motor to spin at idle speed
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_att_sp.thrust_body[0] = (_landed) ? min(_param_fw_thr_idle.get(), 1.f) : get_tecs_thrust();
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}
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/* Copy thrust and pitch values from tecs */
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_att_sp.pitch_body = get_tecs_pitch();
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if (!_vehicle_status.in_transition_to_fw) {
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publishLocalPositionSetpoint(current_sp);
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}
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}
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void
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FixedwingPositionControl::control_auto_fixed_bank_alt_hold(const float control_interval)
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{
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@ -1017,6 +966,8 @@ void
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FixedwingPositionControl::control_auto_position(const float control_interval, const Vector2d &curr_pos,
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const Vector2f &ground_speed, const position_setpoint_s &pos_sp_prev, const position_setpoint_s &pos_sp_curr)
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{
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move_position_setpoint_for_vtol_transition(pos_sp_curr);
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const float acc_rad = _npfg.switchDistance(500.0f);
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Vector2d curr_wp{0, 0};
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Vector2d prev_wp{0, 0};
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@ -1118,6 +1069,19 @@ FixedwingPositionControl::control_auto_position(const float control_interval, co
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tecs_fw_thr_max,
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_param_sinkrate_target.get(),
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_param_climbrate_target.get());
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if (_landed) {
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_att_sp.thrust_body[0] = _param_fw_thr_min.get();
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} else {
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_att_sp.thrust_body[0] = min(get_tecs_thrust(), _param_fw_thr_max.get());
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}
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_att_sp.pitch_body = get_tecs_pitch();
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if (!_vehicle_status.in_transition_to_fw) {
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publishLocalPositionSetpoint(pos_sp_curr);
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}
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}
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void
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@ -1176,6 +1140,8 @@ FixedwingPositionControl::control_auto_loiter(const float control_interval, cons
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const Vector2f &ground_speed, const position_setpoint_s &pos_sp_prev, const position_setpoint_s &pos_sp_curr,
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const position_setpoint_s &pos_sp_next)
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{
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move_position_setpoint_for_vtol_transition(pos_sp_curr);
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Vector2d curr_wp{0, 0};
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Vector2d prev_wp{0, 0};
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@ -1275,6 +1241,20 @@ FixedwingPositionControl::control_auto_loiter(const float control_interval, cons
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tecs_fw_thr_max,
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_param_sinkrate_target.get(),
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_param_climbrate_target.get());
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if (_landed) {
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_att_sp.thrust_body[0] = _param_fw_thr_min.get();
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} else {
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_att_sp.thrust_body[0] = min(get_tecs_thrust(), _param_fw_thr_max.get());
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}
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_att_sp.pitch_body = get_tecs_pitch();
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if (!_vehicle_status.in_transition_to_fw) {
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publishLocalPositionSetpoint(pos_sp_curr);
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}
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}
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void
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@ -2313,12 +2293,6 @@ FixedwingPositionControl::Run()
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_new_landing_gear_position = landing_gear_s::GEAR_KEEP; // is overwritten in Takeoff and Land
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switch (_control_mode_current) {
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case FW_POSCTRL_MODE_AUTO: {
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control_auto(control_interval, curr_pos, ground_speed, _pos_sp_triplet.previous, _pos_sp_triplet.current,
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_pos_sp_triplet.next);
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break;
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}
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case FW_POSCTRL_MODE_AUTO_ALTITUDE: {
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control_auto_fixed_bank_alt_hold(control_interval);
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break;
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@ -2340,6 +2314,17 @@ FixedwingPositionControl::Run()
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break;
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}
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case FW_POSCTRL_MODE_AUTO_LOITER: {
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control_auto_loiter(control_interval, curr_pos, ground_speed, _pos_sp_triplet.previous, _pos_sp_triplet.current,
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_pos_sp_triplet.next);
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break;
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}
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case FW_POSCTRL_MODE_AUTO_POSITION: {
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control_auto_position(control_interval, curr_pos, ground_speed, _pos_sp_triplet.previous, _pos_sp_triplet.current);
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break;
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}
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case FW_POSCTRL_MODE_AUTO_TAKEOFF: {
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control_auto_takeoff(_local_pos.timestamp, control_interval, curr_pos, ground_speed, _pos_sp_triplet.current);
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break;
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@ -168,12 +168,13 @@ static constexpr float MANUAL_TOUCHDOWN_NUDGE_INPUT_DEADZONE = 0.15f;
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static constexpr float POST_TOUCHDOWN_CLAMP_TIME = 0.5f;
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enum FW_POSCTRL_MODE {
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FW_POSCTRL_MODE_AUTO,
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FW_POSCTRL_MODE_AUTO_ALTITUDE,
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FW_POSCTRL_MODE_AUTO_CLIMBRATE,
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FW_POSCTRL_MODE_AUTO_TAKEOFF,
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FW_POSCTRL_MODE_AUTO_LANDING_STRAIGHT,
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FW_POSCTRL_MODE_AUTO_LANDING_CIRCULAR,
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FW_POSCTRL_MODE_AUTO_LOITER,
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FW_POSCTRL_MODE_AUTO_POSITION,
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FW_POSCTRL_MODE_AUTO_VELOCITY,
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FW_POSCTRL_MODE_MANUAL_POSITION,
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FW_POSCTRL_MODE_MANUAL_ALTITUDE,
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@ -532,19 +533,6 @@ private:
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/* automatic control methods */
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/**
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* @brief Automatic position control for waypoints, orbits, and velocity control
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*
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* @param control_interval Time since last position control call [s]
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* @param curr_pos Current 2D local position vector of vehicle [m]
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* @param ground_speed Local 2D ground speed of vehicle [m/s]
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* @param pos_sp_prev previous position setpoint
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* @param pos_sp_curr current position setpoint
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* @param pos_sp_next next position setpoint
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*/
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void control_auto(const float control_interval, const Vector2d &curr_pos, const Vector2f &ground_speed,
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const position_setpoint_s &pos_sp_prev, const position_setpoint_s &pos_sp_curr, const position_setpoint_s &pos_sp_next);
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/**
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* @brief Controls altitude and airspeed for a fixed-bank loiter.
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*
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