2014-01-30 08:13:17 -04:00
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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_acro.pde - init and run calls for acro flight mode for trad heli
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*/
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// heli_acro_init - initialise acro controller
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static bool heli_acro_init(bool ignore_checks)
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{
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2014-06-06 00:05:09 -03:00
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// always successfully enter acro
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2014-01-30 08:13:17 -04:00
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return true;
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}
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// heli_acro_run - runs the acro controller
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// should be called at 100hz or more
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static void heli_acro_run()
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{
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2014-02-09 21:50:43 -04:00
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float target_roll, target_pitch, target_yaw;
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2014-01-30 20:55:20 -04:00
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int16_t pilot_throttle_scaled;
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2014-01-30 08:13:17 -04:00
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2014-01-30 08:45:01 -04:00
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// if not armed or main rotor not up to full speed clear stabilized rate errors
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// unlike multicopters we do not set throttle (i.e. collective pitch) to zero so the swash servos move
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if(!motors.armed() || !motors.motor_runup_complete()) {
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2014-06-06 00:05:09 -03:00
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attitude_control.relax_bf_rate_controller();
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2014-06-06 02:46:02 -03:00
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attitude_control.set_yaw_target_to_current_heading();
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2014-01-30 08:45:01 -04:00
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}
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2014-01-30 08:13:17 -04:00
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// To-Do: add support for flybarred helis
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// convert the input to the desired body frame rate
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get_pilot_desired_angle_rates(g.rc_1.control_in, g.rc_2.control_in, g.rc_4.control_in, target_roll, target_pitch, target_yaw);
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2014-01-30 20:55:20 -04:00
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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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// run attitude controller
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2014-02-13 22:53:21 -04:00
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attitude_control.rate_bf_roll_pitch_yaw(target_roll, target_pitch, target_yaw);
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2014-01-30 20:55:20 -04:00
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// output pilot's throttle without angle boost
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attitude_control.set_throttle_out(pilot_throttle_scaled, false);
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2014-01-30 08:13:17 -04:00
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}
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#endif //HELI_FRAME
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