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• This comparison shows the changes necessary to convert path

  → /branches/dongfang_FC_fixedwing/arduino_atmega328/flight.c @ 2140

  → /branches/dongfang_FC_fixedwing/arduino_atmega328/flight.c @ 2141

  ↔ Reverse comparison

• Compare Path:	Rev

  With Path:	Rev

Ignore whitespace Rev 2140 → Rev 2141

/branches/dongfang_FC_fixedwing/arduino_atmega328/flight.c
165,8 → 165,6
}
#endif
debugOut.analog[9+axis] = error / (GYRO_DEG_FACTOR / 10); // in 0.1 deg
/************************************************************************/
/* Calculate control feedback from angle (gyro integral) */
/* and angular velocity (gyro signal) */
243,10 → 241,5
debugOut.analog[13] = term[ROLL];
debugOut.analog[14] = term[YAW];
debugOut.analog[15] = term[THROTTLE];
//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
}
}