mirror of https://github.com/ArduPilot/ardupilot
AC_AttitudeControl: Heli: invert throttle in inverted flight, move state down to heli
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24c843dc26
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@ -566,9 +566,6 @@ protected:
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void control_monitor_filter_pid(float value, float &rms_P);
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void control_monitor_filter_pid(float value, float &rms_P);
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void control_monitor_update(void);
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void control_monitor_update(void);
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// true in inverted flight mode
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bool _inverted_flight;
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public:
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public:
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// log a CTRL message
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// log a CTRL message
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void control_monitor_log(void) const;
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void control_monitor_log(void) const;
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@ -538,6 +538,11 @@ void AC_AttitudeControl_Heli::set_throttle_out(float throttle_in, bool apply_ang
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{
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{
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_throttle_in = throttle_in;
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_throttle_in = throttle_in;
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update_althold_lean_angle_max(throttle_in);
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update_althold_lean_angle_max(throttle_in);
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if (_inverted_flight) {
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throttle_in = 1.0 - throttle_in;
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}
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_motors.set_throttle_filter_cutoff(filter_cutoff);
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_motors.set_throttle_filter_cutoff(filter_cutoff);
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_motors.set_throttle(throttle_in);
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_motors.set_throttle(throttle_in);
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// Clear angle_boost for logging purposes
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// Clear angle_boost for logging purposes
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@ -101,6 +101,9 @@ private:
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uint8_t tail_passthrough : 1; // 1 if we should pass through pilots yaw input to tail
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uint8_t tail_passthrough : 1; // 1 if we should pass through pilots yaw input to tail
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} _flags_heli;
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} _flags_heli;
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// true in inverted flight mode
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bool _inverted_flight;
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// Integrate vehicle rate into _att_error_rot_vec_rad
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// Integrate vehicle rate into _att_error_rot_vec_rad
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void integrate_bf_rate_error_to_angle_errors();
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void integrate_bf_rate_error_to_angle_errors();
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