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)
|
|
|
|
{
|
2014-06-06 00:05:09 -03:00
|
|
|
// always successfully enter acro
|
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()
|
|
|
|
{
|
2014-02-09 21:50:43 -04:00
|
|
|
float target_roll, target_pitch, target_yaw;
|
2014-05-11 13:21:27 -03:00
|
|
|
static bool init_targets_on_arming;
|
|
|
|
|
|
|
|
// Tradheli should not reset roll, pitch, yaw targets when motors are not runup, because
|
|
|
|
// we may be in autorotation flight. These should be reset only when transitioning from disarmed
|
|
|
|
// to armed, because the pilot will have placed the helicopter down on the landing pad. This is so
|
|
|
|
// that the servos move in a realistic fashion while disarmed for operational checks.
|
|
|
|
// Also, unlike multicopters we do not set throttle (i.e. collective pitch) to zero so the swash servos move
|
|
|
|
|
|
|
|
if(!motors.armed()) {
|
|
|
|
init_targets_on_arming=true;
|
2014-06-06 02:46:02 -03:00
|
|
|
attitude_control.set_yaw_target_to_current_heading();
|
2014-01-30 08:45:01 -04:00
|
|
|
}
|
|
|
|
|
2014-05-11 13:21:27 -03:00
|
|
|
if(motors.armed() && init_targets_on_arming) {
|
|
|
|
init_targets_on_arming=false;
|
|
|
|
attitude_control.relax_bf_rate_controller();
|
|
|
|
|
|
|
|
}
|
|
|
|
|
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);
|
|
|
|
|
2014-01-30 20:55:20 -04:00
|
|
|
// run attitude controller
|
2014-02-13 22:53:21 -04:00
|
|
|
attitude_control.rate_bf_roll_pitch_yaw(target_roll, target_pitch, target_yaw);
|
2014-01-30 20:55:20 -04:00
|
|
|
|
|
|
|
// output pilot's throttle without angle boost
|
2014-05-11 11:49:35 -03:00
|
|
|
attitude_control.set_throttle_out(g.rc_3.control_in, false);
|
2014-01-30 08:13:17 -04:00
|
|
|
}
|
|
|
|
|
|
|
|
#endif //HELI_FRAME
|