mirror of https://github.com/ArduPilot/ardupilot
Sub: Guided Mode: Improved guided_set_velocity() and fixed Z-controller in guided_vel_control_run()
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@ -109,6 +109,9 @@ void ModeGuided::guided_vel_control_start()
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// initialise velocity controller
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position_control->init_z_controller();
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position_control->init_xy_controller();
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// pilot always controls yaw
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set_auto_yaw_mode(AUTO_YAW_HOLD);
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}
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// initialise guided mode's posvel controller
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@ -260,6 +263,24 @@ void ModeGuided::guided_set_velocity(const Vector3f& velocity)
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position_control->set_vel_desired_cms(velocity);
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}
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// guided_set_velocity - sets guided mode's target velocity
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void ModeGuided::guided_set_velocity(const Vector3f& velocity, bool use_yaw, float yaw_cd, bool use_yaw_rate, float yaw_rate_cds, bool relative_yaw)
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{
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// check we are in velocity control mode
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if (sub.guided_mode != Guided_Velocity) {
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guided_vel_control_start();
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}
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// set yaw state
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guided_set_yaw_state(use_yaw, yaw_cd, use_yaw_rate, yaw_rate_cds, relative_yaw);
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update_time_ms = AP_HAL::millis();
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// set position controller velocity target
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position_control->set_vel_desired_cms(velocity);
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}
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// set guided mode posvel target
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bool ModeGuided::guided_set_destination_posvel(const Vector3f& destination, const Vector3f& velocity)
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{
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@ -465,6 +486,12 @@ void ModeGuided::guided_vel_control_run()
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target_yaw_rate = sub.get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
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if (!is_zero(target_yaw_rate)) {
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set_auto_yaw_mode(AUTO_YAW_HOLD);
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} else{
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if (sub.yaw_rate_only){
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set_auto_yaw_mode(AUTO_YAW_RATE);
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} else{
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set_auto_yaw_mode(AUTO_YAW_LOOK_AT_HEADING);
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}
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}
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}
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@ -480,6 +507,8 @@ void ModeGuided::guided_vel_control_run()
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position_control->stop_pos_xy_stabilisation();
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// call velocity controller which includes z axis controller
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position_control->update_xy_controller();
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position_control->set_pos_target_z_from_climb_rate_cm(position_control->get_vel_desired_cms().z);
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position_control->update_z_controller();
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float lateral_out, forward_out;
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@ -493,6 +522,14 @@ void ModeGuided::guided_vel_control_run()
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if (sub.auto_yaw_mode == AUTO_YAW_HOLD) {
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// roll & pitch & yaw rate from pilot
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attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_yaw_rate);
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} else if (sub.auto_yaw_mode == AUTO_YAW_LOOK_AT_HEADING) {
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// roll, pitch from pilot, yaw & yaw_rate from auto_control
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target_yaw_rate = sub.yaw_look_at_heading_slew * 100.0;
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attitude_control->input_euler_angle_roll_pitch_slew_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), get_auto_heading(), target_yaw_rate);
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} else if (sub.auto_yaw_mode == AUTO_YAW_RATE) {
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// roll, pitch from pilot, yaw_rate from auto_control
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target_yaw_rate = sub.yaw_look_at_heading_slew * 100.0;
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attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), target_yaw_rate);
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} else {
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// roll, pitch from pilot, yaw heading from auto_heading()
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attitude_control->input_euler_angle_roll_pitch_yaw(channel_roll->get_control_in(), channel_pitch->get_control_in(), get_auto_heading(), true);
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