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update some comment typos in sensors/acceleration.c

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This commit is contained in:
Dominic Clifton 2014-10-24 18:35:59 +01:00
parent a2a9443045
commit a92b148557
1 changed files with 4 additions and 5 deletions
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9
src/main/sensors/acceleration.c
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@ -130,8 +130,8 @@ void performInflightAccelerationCalibration(rollAndPitchTrims_t *rollAndPitchTri
if (InflightcalibratingA == 1) { if (InflightcalibratingA == 1) {
AccInflightCalibrationActive = false; AccInflightCalibrationActive = false;
AccInflightCalibrationMeasurementDone = true; AccInflightCalibrationMeasurementDone = true;
queueConfirmationBeep(2); // beeper to indicatiing the end of calibration queueConfirmationBeep(2); // beeper to indicating the end of calibration
// recover saved values to maintain current flight behavior until new values are transferred // recover saved values to maintain current flight behaviour until new values are transferred
accelerationTrims->raw[FD_ROLL] = accZero_saved[FD_ROLL]; accelerationTrims->raw[FD_ROLL] = accZero_saved[FD_ROLL];
accelerationTrims->raw[FD_PITCH] = accZero_saved[FD_PITCH]; accelerationTrims->raw[FD_PITCH] = accZero_saved[FD_PITCH];
accelerationTrims->raw[FD_YAW] = accZero_saved[FD_YAW]; accelerationTrims->raw[FD_YAW] = accZero_saved[FD_YAW];
@ -141,17 +141,16 @@ void performInflightAccelerationCalibration(rollAndPitchTrims_t *rollAndPitchTri
InflightcalibratingA--; InflightcalibratingA--;
} }
// Calculate average, shift Z down by acc_1G and store values in EEPROM at end of calibration // 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; AccInflightCalibrationSavetoEEProm = false;
accelerationTrims->raw[FD_ROLL] = b[FD_ROLL] / 50; accelerationTrims->raw[FD_ROLL] = b[FD_ROLL] / 50;
accelerationTrims->raw[FD_PITCH] = b[FD_PITCH] / 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); resetRollAndPitchTrims(rollAndPitchTrims);
saveConfigAndNotify(); saveConfigAndNotify();
} }
} }
void applyAccelerationTrims(flightDynamicsTrims_t *accelerationTrims) void applyAccelerationTrims(flightDynamicsTrims_t *accelerationTrims)