|
|
|
@ -1423,7 +1423,7 @@ void QuadPlane::update_transition(void)
@@ -1423,7 +1423,7 @@ void QuadPlane::update_transition(void)
|
|
|
|
|
// millisecond. Assume we want to get to the transition angle
|
|
|
|
|
// in half the transition time
|
|
|
|
|
float transition_rate = tailsitter.transition_angle / float(transition_time_ms/2); |
|
|
|
|
uint32_t dt = now - transition_low_airspeed_ms; |
|
|
|
|
uint32_t dt = now - transition_start_ms; |
|
|
|
|
plane.nav_pitch_cd = constrain_float((-transition_rate * dt)*100, -8500, 0); |
|
|
|
|
plane.nav_roll_cd = 0; |
|
|
|
|
check_attitude_relax(); |
|
|
|
|