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https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-30 04:06:33 +08:00
VTOL attitude controller: run update_vtol_state only if mc or fw att sp changed, such that pusher support in hover works again
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
committed by
Roman Bapst
parent
1b2403a87f
commit
92b824e218
@@ -354,7 +354,12 @@ VtolAttitudeControl::Run()
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_land_detected_sub.update(&_land_detected);
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_land_detected_sub.update(&_land_detected);
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vehicle_cmd_poll();
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vehicle_cmd_poll();
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// check if mc and fw sp were updated
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bool mc_att_sp_updated = _mc_virtual_att_sp_sub.update(&_mc_virtual_att_sp);
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bool fw_att_sp_updated = _fw_virtual_att_sp_sub.update(&_fw_virtual_att_sp);
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// update the vtol state machine which decides which mode we are in
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// update the vtol state machine which decides which mode we are in
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if (mc_att_sp_updated || fw_att_sp_updated) {
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_vtol_type->update_vtol_state();
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_vtol_type->update_vtol_state();
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// reset transition command if not auto control
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// reset transition command if not auto control
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@@ -372,6 +377,9 @@ VtolAttitudeControl::Run()
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_transition_command = vtol_vehicle_status_s::VEHICLE_VTOL_STATE_MC;
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_transition_command = vtol_vehicle_status_s::VEHICLE_VTOL_STATE_MC;
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}
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}
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}
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}
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}
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// check in which mode we are in and call mode specific functions
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// check in which mode we are in and call mode specific functions
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switch (_vtol_type->get_mode()) {
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switch (_vtol_type->get_mode()) {
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@@ -384,7 +392,7 @@ VtolAttitudeControl::Run()
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_fw_virtual_att_sp_sub.update(&_fw_virtual_att_sp);
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_fw_virtual_att_sp_sub.update(&_fw_virtual_att_sp);
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if (_mc_virtual_att_sp_sub.update(&_mc_virtual_att_sp)) {
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if (mc_att_sp_updated || fw_att_sp_updated) {
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// reinitialize the setpoint while not armed to make sure no value from the last mode or flight is still kept
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// reinitialize the setpoint while not armed to make sure no value from the last mode or flight is still kept
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if (!_v_control_mode.flag_armed) {
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if (!_v_control_mode.flag_armed) {
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@@ -406,9 +414,7 @@ VtolAttitudeControl::Run()
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_vtol_vehicle_status.vtol_in_trans_mode = false;
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_vtol_vehicle_status.vtol_in_trans_mode = false;
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_vtol_vehicle_status.in_transition_to_fw = false;
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_vtol_vehicle_status.in_transition_to_fw = false;
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// got data from mc attitude controller
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if (mc_att_sp_updated) {
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if (_mc_virtual_att_sp_sub.update(&_mc_virtual_att_sp)) {
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// reinitialize the setpoint while not armed to make sure no value from the last mode or flight is still kept
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// reinitialize the setpoint while not armed to make sure no value from the last mode or flight is still kept
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if (!_v_control_mode.flag_armed) {
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if (!_v_control_mode.flag_armed) {
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Quatf().copyTo(_mc_virtual_att_sp.q_d);
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Quatf().copyTo(_mc_virtual_att_sp.q_d);
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@@ -416,10 +422,10 @@ VtolAttitudeControl::Run()
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Quatf().copyTo(_v_att_sp.q_d);
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Quatf().copyTo(_v_att_sp.q_d);
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Vector3f().copyTo(_v_att_sp.thrust_body);
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Vector3f().copyTo(_v_att_sp.thrust_body);
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}
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}
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}
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_vtol_type->update_mc_state();
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_vtol_type->update_mc_state();
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_v_att_sp_pub.publish(_v_att_sp);
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_v_att_sp_pub.publish(_v_att_sp);
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}
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break;
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break;
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@@ -429,7 +435,7 @@ VtolAttitudeControl::Run()
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_vtol_vehicle_status.vtol_in_trans_mode = false;
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_vtol_vehicle_status.vtol_in_trans_mode = false;
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_vtol_vehicle_status.in_transition_to_fw = false;
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_vtol_vehicle_status.in_transition_to_fw = false;
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if (_fw_virtual_att_sp_sub.update(&_fw_virtual_att_sp)) {
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if (fw_att_sp_updated) {
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_vtol_type->update_fw_state();
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_vtol_type->update_fw_state();
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_v_att_sp_pub.publish(_v_att_sp);
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_v_att_sp_pub.publish(_v_att_sp);
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}
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}
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