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• This comparison shows the changes necessary to convert path

  → /branches/dongfang_FC_fixedwing/analog.c @ 2123

  → /branches/dongfang_FC_fixedwing/analog.c @ 2124

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Ignore whitespace Rev 2123 → Rev 2124

/branches/dongfang_FC_fixedwing/analog.c
412,7 → 412,7
// determine gyro bias by averaging (requires that the aircraft does not rotate around any axis!)
for (i = 0; i < OFFSET_CYCLES; i++) {
delay_ms_with_adc_measurement(2, 1);
delay_ms_with_adc_measurement(4, 1);
for (axis = PITCH; axis <= YAW; axis++) {
offsets[axis] += rawGyroValue(axis);
}