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• This comparison shows the changes necessary to convert path

  → /branches/dongfang_FC_fixedwing/flight.c @ 1921

  → /branches/dongfang_FC_fixedwing/flight.c @ 1922

  ↔ Reverse comparison

• Compare Path:	Rev

  With Path:	Rev

Ignore whitespace Rev 1921 → Rev 1922

/branches/dongfang_FC_fixedwing/flight.c
139,7 → 139,6
}
/************************************************************************/
/* Calculate control feedback from angle (gyro integral) */
/* and angular velocity (gyro signal) */
/************************************************************************/
154,7 → 153,9
PDPartYaw = (int32_t) (yawRate * 2 * (int32_t) yawPFactor) / (256L / CONTROL_SCALING)
+ (differential[YAW] * (int16_t) dynamicParams.GyroYawD) / 16;
/************************************************************************/
/* Stick signals are positive and gyros are negative... */
/************************************************************************/
IPart[PITCH] = controlIntegrals[CONTROL_ELEVATOR] - angle[PITCH];
if (IPart[PITCH] > PITCHROLLOVER180) IPart[PITCH] -= PITCHROLLOVER360;
else if (IPart[PITCH] <= -PITCHROLLOVER180) IPart[PITCH] += PITCHROLLOVER360;