/branches/dongfang_FC_fixedwing/flight.c |
---|
68,9 → 68,9 |
return pid; |
} |
uint16_t result = (pid * 10) / airspeed; |
uint16_t result = (pid * 10) / airspeedVelocity; |
if (result > 240 || airspeed == 0) { |
if (result > 240 || airspeedVelocity == 0) { |
result = 240; |
} |