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