diff --git a/src/main/sensors/acceleration.c b/src/main/sensors/acceleration.c index 6a8c09869d..e8ce78b304 100644 --- a/src/main/sensors/acceleration.c +++ b/src/main/sensors/acceleration.c @@ -130,8 +130,8 @@ void performInflightAccelerationCalibration(rollAndPitchTrims_t *rollAndPitchTri if (InflightcalibratingA == 1) { AccInflightCalibrationActive = false; AccInflightCalibrationMeasurementDone = true; - queueConfirmationBeep(2); // beeper to indicatiing the end of calibration - // recover saved values to maintain current flight behavior until new values are transferred + queueConfirmationBeep(2); // beeper to indicating the end of calibration + // recover saved values to maintain current flight behaviour until new values are transferred accelerationTrims->raw[FD_ROLL] = accZero_saved[FD_ROLL]; accelerationTrims->raw[FD_PITCH] = accZero_saved[FD_PITCH]; accelerationTrims->raw[FD_YAW] = accZero_saved[FD_YAW]; @@ -141,17 +141,16 @@ void performInflightAccelerationCalibration(rollAndPitchTrims_t *rollAndPitchTri InflightcalibratingA--; } // Calculate average, shift Z down by acc_1G and store values in EEPROM at end of calibration - if (AccInflightCalibrationSavetoEEProm) { // the copter is landed, disarmed and the combo has been done again + if (AccInflightCalibrationSavetoEEProm) { // the aircraft is landed, disarmed and the combo has been done again AccInflightCalibrationSavetoEEProm = false; accelerationTrims->raw[FD_ROLL] = b[FD_ROLL] / 50; accelerationTrims->raw[FD_PITCH] = b[FD_PITCH] / 50; - accelerationTrims->raw[FD_YAW] = b[FD_YAW] / 50 - acc_1G; // for nunchuk 200=1G + accelerationTrims->raw[FD_YAW] = b[FD_YAW] / 50 - acc_1G; // for nunchuck 200=1G resetRollAndPitchTrims(rollAndPitchTrims); saveConfigAndNotify(); } - } void applyAccelerationTrims(flightDynamicsTrims_t *accelerationTrims)