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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- |
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#if FRAME_CONFIG == HELI_FRAME |
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/* |
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* heli_control_stabilize.pde - init and run calls for stabilize flight mode for trad heli |
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*/ |
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// stabilize_init - initialise stabilize controller |
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static bool heli_stabilize_init(bool ignore_checks) |
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{ |
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// set target altitude to zero for reporting |
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// To-Do: make pos controller aware when it's active/inactive so it can always report the altitude error? |
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pos_control.set_alt_target(0); |
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return true; |
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} |
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// stabilize_run - runs the main stabilize controller |
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// should be called at 100hz or more |
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static void heli_stabilize_run() |
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{ |
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int16_t target_roll, target_pitch; |
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float target_yaw_rate; |
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int16_t pilot_throttle_scaled; |
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// To-Do: should tradheli reset roll, pitch, yaw targets when motors are not runup? |
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// apply SIMPLE mode transform to pilot inputs |
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update_simple_mode(); |
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// convert pilot input to lean angles |
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// To-Do: convert get_pilot_desired_lean_angles to return angles as floats |
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get_pilot_desired_lean_angles(g.rc_1.control_in, g.rc_2.control_in, target_roll, target_pitch); |
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// get pilot's desired yaw rate |
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target_yaw_rate = get_pilot_desired_yaw_rate(g.rc_4.control_in); |
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// get pilot's desired throttle |
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pilot_throttle_scaled = get_pilot_desired_throttle(g.rc_3.control_in); |
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// call attitude controller |
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attitude_control.angleef_rp_rateef_y(target_roll, target_pitch, target_yaw_rate); |
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// output pilot's throttle - note that TradHeli does not used angle-boost |
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attitude_control.set_throttle_out(pilot_throttle_scaled, false); |
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// re-fetch angle targets for reporting |
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const Vector3f angle_target = attitude_control.angle_ef_targets(); |
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control_roll = angle_target.x; |
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control_pitch = angle_target.y; |
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control_yaw = angle_target.z; |
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// update estimate of throttle cruise |
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update_throttle_cruise(motors.get_collective_out()); |
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} |
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#endif //HELI_FRAME |
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