|
|
|
@ -5,7 +5,11 @@
@@ -5,7 +5,11 @@
|
|
|
|
|
*/ |
|
|
|
|
|
|
|
|
|
#ifndef DRIFT_SPEEDGAIN |
|
|
|
|
# define DRIFT_SPEEDGAIN 14.0 |
|
|
|
|
# define DRIFT_SPEEDGAIN 14.0f |
|
|
|
|
#endif |
|
|
|
|
|
|
|
|
|
#ifndef DRIFT_THR_GAIN |
|
|
|
|
# define DRIFT_THR_GAIN 2.0f |
|
|
|
|
#endif |
|
|
|
|
|
|
|
|
|
// drift_init - initialise drift controller |
|
|
|
@ -27,8 +31,8 @@ static void drift_run()
@@ -27,8 +31,8 @@ static void drift_run()
|
|
|
|
|
float target_yaw_rate; |
|
|
|
|
int16_t pilot_throttle_scaled; |
|
|
|
|
|
|
|
|
|
// if not armed or landed, set throttle to zero and exit immediately |
|
|
|
|
if(!motors.armed() || ap.land_complete) { |
|
|
|
|
// if not armed or landed and throttle at zero, set throttle to zero and exit immediately |
|
|
|
|
if(!motors.armed() || (ap.land_complete && g.rc_3.control_in <= 0)) { |
|
|
|
|
attitude_control.init_targets(); |
|
|
|
|
attitude_control.set_throttle_out(0, false); |
|
|
|
|
return; |
|
|
|
@ -68,9 +72,13 @@ static void drift_run()
@@ -68,9 +72,13 @@ static void drift_run()
|
|
|
|
|
breaker = 0.0; |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
// throttle assist |
|
|
|
|
float thr_assist = 1.0 - ((float)abs(pilot_throttle_scaled - 500) / 200.0); |
|
|
|
|
thr_assist = max(thr_assist, 0) * -DRIFT_THR_GAIN * vel.z; |
|
|
|
|
|
|
|
|
|
// call attitude controller |
|
|
|
|
attitude_control.angle_ef_roll_pitch_rate_ef_yaw_smooth(target_roll, target_pitch, target_yaw_rate, get_smoothing_gain()); |
|
|
|
|
|
|
|
|
|
// output pilot's throttle with angle boost |
|
|
|
|
attitude_control.set_throttle_out(pilot_throttle_scaled, true); |
|
|
|
|
attitude_control.set_throttle_out(pilot_throttle_scaled + thr_assist, true); |
|
|
|
|
} |
|
|
|
|