ardupilot/ArduCopter/heli_control_acro.pde

44 lines
1.4 KiB
Plaintext
Raw Normal View History

2014-01-30 08:13:17 -04:00
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#if FRAME_CONFIG == HELI_FRAME
/*
* heli_control_acro.pde - init and run calls for acro flight mode for trad heli
*/
// heli_acro_init - initialise acro controller
static bool heli_acro_init(bool ignore_checks)
{
// clear stabilized rate errors
attitude_control.init_targets();
2014-01-30 08:13:17 -04:00
return true;
}
// heli_acro_run - runs the acro controller
// should be called at 100hz or more
static void heli_acro_run()
{
int16_t target_roll, target_pitch, target_yaw;
int16_t pilot_throttle_scaled;
2014-01-30 08:13:17 -04:00
// if not armed or main rotor not up to full speed clear stabilized rate errors
// unlike multicopters we do not set throttle (i.e. collective pitch) to zero so the swash servos move
if(!motors.armed() || !motors.motor_runup_complete()) {
attitude_control.init_targets();
}
2014-01-30 08:13:17 -04:00
// To-Do: add support for flybarred helis
// convert the input to the desired body frame rate
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);
// get pilot's desired throttle
pilot_throttle_scaled = get_pilot_desired_throttle(g.rc_3.control_in);
// run attitude controller
2014-01-30 08:13:17 -04:00
attitude_control.ratebf_rpy(target_roll, target_pitch, target_yaw);
// output pilot's throttle without angle boost
attitude_control.set_throttle_out(pilot_throttle_scaled, false);
2014-01-30 08:13:17 -04:00
}
#endif //HELI_FRAME