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mc_att_control: don't store full vehicle_land_detected copy
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@@ -104,7 +104,7 @@ MulticopterAttitudeControl::parameters_updated()
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float
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MulticopterAttitudeControl::throttle_curve(float throttle_stick_input)
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{
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const float throttle_min = _vehicle_land_detected.landed ? 0.0f : _param_mpc_manthr_min.get();
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const float throttle_min = _landed ? 0.0f : _param_mpc_manthr_min.get();
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// throttle_stick_input is in range [0, 1]
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switch (_param_mpc_thr_curve.get()) {
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@@ -268,7 +268,15 @@ MulticopterAttitudeControl::Run()
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/* check for updates in other topics */
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_manual_control_setpoint_sub.update(&_manual_control_setpoint);
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_v_control_mode_sub.update(&_v_control_mode);
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_vehicle_land_detected_sub.update(&_vehicle_land_detected);
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if (_vehicle_land_detected_sub.updated()) {
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vehicle_land_detected_s vehicle_land_detected;
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if (_vehicle_land_detected_sub.copy(&vehicle_land_detected)) {
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_landed = vehicle_land_detected.landed;
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}
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}
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_vehicle_status_sub.update(&_vehicle_status);
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/* Check if we are in rattitude mode and the pilot is above the threshold on pitch
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@@ -334,8 +342,7 @@ MulticopterAttitudeControl::Run()
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// reset yaw setpoint during transitions, tailsitter.cpp generates
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// attitude setpoint for the transition
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_reset_yaw_sp = (!attitude_setpoint_generated && !_v_control_mode.flag_control_rattitude_enabled) ||
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_vehicle_land_detected.landed ||
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(_vehicle_status.is_vtol && _vehicle_status.in_transition_mode);
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_landed || (_vehicle_status.is_vtol && _vehicle_status.in_transition_mode);
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}
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