| /branches/dongfang_FC_fixedwing/flight.c |
|---|
| 264,10 → 264,5 |
| debugOut.analog[12] = term[PITCH]; |
| debugOut.analog[13] = term[ROLL]; |
| debugOut.analog[14] = term[YAW]; |
| //DebugOut.Analog[18] = (10 * controlIntegrals[CONTROL_ELEVATOR]) / GYRO_DEG_FACTOR_PITCHROLL; // in 0.1 deg |
| //DebugOut.Analog[19] = (10 * controlIntegrals[CONTROL_AILERONS]) / GYRO_DEG_FACTOR_PITCHROLL; // in 0.1 deg |
| //debugOut.analog[22] = (10 * IPart[PITCH]) / GYRO_DEG_FACTOR; // in 0.1 deg |
| //debugOut.analog[23] = (10 * IPart[ROLL]) / GYRO_DEG_FACTOR; // in 0.1 deg |
| } |
| } |