Plane: Qstabilize: mode functions to ModeQStabilize
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@ -10,6 +10,12 @@ bool ModeQStabilize::_enter()
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return true;
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}
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// init quadplane stabilize mode
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void ModeQStabilize::init()
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{
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quadplane.throttle_wait = false;
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}
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void ModeQStabilize::update()
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{
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// set nav_roll and nav_pitch using sticks
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@ -38,6 +44,20 @@ void ModeQStabilize::update()
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}
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}
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// quadplane stabilize mode
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void ModeQStabilize::run()
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{
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// special check for ESC calibration in QSTABILIZE
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if (quadplane.esc_calibration != 0) {
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quadplane.run_esc_calibration();
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return;
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}
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// normal QSTABILIZE mode
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float pilot_throttle_scaled = quadplane.get_pilot_throttle();
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quadplane.hold_stabilize(pilot_throttle_scaled);
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}
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// set the desired roll and pitch for a tailsitter
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void ModeQStabilize::set_tailsitter_roll_pitch(const float roll_input, const float pitch_input)
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{
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@ -845,13 +845,6 @@ void QuadPlane::run_esc_calibration(void)
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}
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}
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// init quadplane stabilize mode
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void ModeQStabilize::init()
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{
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quadplane.throttle_wait = false;
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}
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/*
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when doing a forward transition of a tilt-vectored quadplane we use
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euler angle control to maintain good yaw. This updates the yaw
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@ -997,20 +990,6 @@ void QuadPlane::hold_stabilize(float throttle_in)
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}
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}
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// quadplane stabilize mode
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void ModeQStabilize::run()
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{
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// special check for ESC calibration in QSTABILIZE
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if (quadplane.esc_calibration != 0) {
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quadplane.run_esc_calibration();
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return;
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}
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// normal QSTABILIZE mode
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float pilot_throttle_scaled = quadplane.get_pilot_throttle();
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quadplane.hold_stabilize(pilot_throttle_scaled);
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}
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// run the multicopter Z controller
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void QuadPlane::run_z_controller(void)
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{
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