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is_vtol flag in vehicle_status
Getting rid of the autostart based checks if the system is a vtol Fixes #1503
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@@ -338,6 +338,9 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() :
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_actuators_0_pub(-1),
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_actuators_2_pub(-1),
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_rates_sp_id(ORB_ID(vehicle_rates_setpoint)),
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_actuators_id(ORB_ID(actuator_controls_0)),
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/* performance counters */
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_loop_perf(perf_alloc(PC_ELAPSED, "fw att control")),
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_nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control nonfinite input")),
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@@ -400,15 +403,6 @@ FixedwingAttitudeControl::FixedwingAttitudeControl() :
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/* fetch initial parameter values */
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parameters_update();
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// set correct uORB ID, depending on if vehicle is VTOL or not
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if (_parameters.autostart_id >= 13000 && _parameters.autostart_id <= 13999) { /* VTOL airframe?*/
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_rates_sp_id = ORB_ID(fw_virtual_rates_setpoint);
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_actuators_id = ORB_ID(actuator_controls_virtual_fw);
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}
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else {
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_rates_sp_id = ORB_ID(vehicle_rates_setpoint);
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_actuators_id = ORB_ID(actuator_controls_0);
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}
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}
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FixedwingAttitudeControl::~FixedwingAttitudeControl()
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@@ -600,6 +594,14 @@ FixedwingAttitudeControl::vehicle_status_poll()
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if (vehicle_status_updated) {
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orb_copy(ORB_ID(vehicle_status), _vehicle_status_sub, &_vehicle_status);
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/* set correct uORB ID, depending on if vehicle is VTOL or not */
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if (_vehicle_status.is_vtol) {
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_rates_sp_id = ORB_ID(fw_virtual_rates_setpoint);
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_actuators_id = ORB_ID(actuator_controls_virtual_fw);
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} else {
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_rates_sp_id = ORB_ID(vehicle_rates_setpoint);
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_actuators_id = ORB_ID(actuator_controls_0);
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}
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}
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}
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@@ -700,11 +702,11 @@ FixedwingAttitudeControl::task_main()
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/* load local copies */
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orb_copy(ORB_ID(vehicle_attitude), _att_sub, &_att);
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if (_parameters.autostart_id >= 13000
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&& _parameters.autostart_id <= 13999) { //vehicle type is VTOL, need to modify attitude!
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/* The following modification to the attitude is vehicle specific and in this case applies
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to tail-sitter models !!!
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if (_vehicle_status.is_vtol) {
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/* vehicle type is VTOL, need to modify attitude!
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* The following modification to the attitude is vehicle specific and in this case applies
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* to tail-sitter models !!!
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*
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* Since the VTOL airframe is initialized as a multicopter we need to
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* modify the estimated attitude for the fixed wing operation.
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* Since the neutral position of the vehicle in fixed wing mode is -90 degrees rotated around
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@@ -849,7 +851,7 @@ FixedwingAttitudeControl::task_main()
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_yaw_ctrl.reset_integrator();
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}
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} else if (_vcontrol_mode.flag_control_velocity_enabled) {
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/*
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/*
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* Velocity should be controlled and manual is enabled.
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*/
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roll_sp = (_manual.y * _parameters.man_roll_max - _parameters.trim_roll)
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