/branches/dongfang_FC_rewrite/flight.c |
---|
181,6 → 181,7 |
// Fire the main flight attitude calculation, including integration of angles. |
calculateFlightAttitude(); |
J5HIGH; |
throttleTerm = controlThrottle; |
// This check removed. Is done on a per-motor basis, after output matrix multiplication. |
if(throttleTerm < staticParams.MinThrottle + 10) throttleTerm = staticParams.MinThrottle + 10; |
486,4 → 487,5 |
DebugOut.Analog[31] = gyroNoisePeak[ROLL]; |
*/ |
} |
J5LOW; |
} |