@ -529,12 +529,12 @@ void AP_MotorsHeli_Dual::move_actuators(float roll_out, float pitch_out, float c
@@ -529,12 +529,12 @@ void AP_MotorsHeli_Dual::move_actuators(float roll_out, float pitch_out, float c
_rotor . set_motor_load ( fabsf ( collective_out - _collective_mid_pct ) ) ;
// swashplate servos
float servo1_out = ( _rollFactor [ CH_1 ] * roll_out + _pitchFactor [ CH_1 ] * pitch_out + _yawFactor [ CH_1 ] * yaw_out ) / 0.45f + _collectiveFactor [ CH_1 ] * collective_out_scaled ;
float servo2_out = ( _rollFactor [ CH_2 ] * roll_out + _pitchFactor [ CH_2 ] * pitch_out + _yawFactor [ CH_2 ] * yaw_out ) / 0.45f + _collectiveFactor [ CH_2 ] * collective_out_scaled ;
float servo3_out = ( _rollFactor [ CH_3 ] * roll_out + _pitchFactor [ CH_3 ] * pitch_out + _yawFactor [ CH_3 ] * yaw_out ) / 0.45f + _collectiveFactor [ CH_3 ] * collective_out_scaled ;
float servo4_out = ( _rollFactor [ CH_4 ] * roll_out + _pitchFactor [ CH_4 ] * pitch_out + _yawFactor [ CH_4 ] * yaw_out ) / 0.45f + _collectiveFactor [ CH_4 ] * collective2_out_scaled ;
float servo5_out = ( _rollFactor [ CH_5 ] * roll_out + _pitchFactor [ CH_5 ] * pitch_out + _yawFactor [ CH_5 ] * yaw_out ) / 0.45f + _collectiveFactor [ CH_5 ] * collective2_out_scaled ;
float servo6_out = ( _rollFactor [ CH_6 ] * roll_out + _pitchFactor [ CH_6 ] * pitch_out + _yawFactor [ CH_6 ] * yaw_out ) / 0.45f + _collectiveFactor [ CH_6 ] * collective2_out_scaled ;
float servo1_out = ( _rollFactor [ CH_1 ] * roll_out + _pitchFactor [ CH_1 ] * pitch_out + _yawFactor [ CH_1 ] * yaw_out ) * 0.45f + _collectiveFactor [ CH_1 ] * collective_out_scaled ;
float servo2_out = ( _rollFactor [ CH_2 ] * roll_out + _pitchFactor [ CH_2 ] * pitch_out + _yawFactor [ CH_2 ] * yaw_out ) * 0.45f + _collectiveFactor [ CH_2 ] * collective_out_scaled ;
float servo3_out = ( _rollFactor [ CH_3 ] * roll_out + _pitchFactor [ CH_3 ] * pitch_out + _yawFactor [ CH_3 ] * yaw_out ) * 0.45f + _collectiveFactor [ CH_3 ] * collective_out_scaled ;
float servo4_out = ( _rollFactor [ CH_4 ] * roll_out + _pitchFactor [ CH_4 ] * pitch_out + _yawFactor [ CH_4 ] * yaw_out ) * 0.45f + _collectiveFactor [ CH_4 ] * collective2_out_scaled ;
float servo5_out = ( _rollFactor [ CH_5 ] * roll_out + _pitchFactor [ CH_5 ] * pitch_out + _yawFactor [ CH_5 ] * yaw_out ) * 0.45f + _collectiveFactor [ CH_5 ] * collective2_out_scaled ;
float servo6_out = ( _rollFactor [ CH_6 ] * roll_out + _pitchFactor [ CH_6 ] * pitch_out + _yawFactor [ CH_6 ] * yaw_out ) * 0.45f + _collectiveFactor [ CH_6 ] * collective2_out_scaled ;
// rescale from -1..1, so we can use the pwm calc that includes trim
servo1_out = 2 * servo1_out - 1 ;