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Scale acc value in acc sensor code

This commit is contained in:
Martin Budden 2017-11-28 06:50:43 +00:00
parent 61f895333b
commit 089680ffce
7 changed files with 41 additions and 39 deletions

View file

@ -69,6 +69,8 @@ FASTRAM acc_t acc; // acc access functions
static uint16_t calibratingA = 0; // the calibration is done is the main loop. Calibrating decreases at each cycle down to 0, then we enter in a normal mode.
STATIC_FASTRAM int32_t accADC[XYZ_AXIS_COUNT];
STATIC_FASTRAM biquadFilter_t accFilter[XYZ_AXIS_COUNT];
#ifdef USE_ACC_NOTCH
@ -376,7 +378,7 @@ int getPrimaryAxisIndex(int32_t sample[3])
static void performAcclerationCalibration(void)
{
int axisIndex = getPrimaryAxisIndex(acc.accADC);
int axisIndex = getPrimaryAxisIndex(accADC);
// Check if sample is usable
if (axisIndex < 0) {
@ -398,10 +400,10 @@ static void performAcclerationCalibration(void)
}
if (!calibratedAxis[axisIndex]) {
sensorCalibrationPushSampleForOffsetCalculation(&calState, acc.accADC);
accSamples[axisIndex][X] += acc.accADC[X];
accSamples[axisIndex][Y] += acc.accADC[Y];
accSamples[axisIndex][Z] += acc.accADC[Z];
sensorCalibrationPushSampleForOffsetCalculation(&calState, accADC);
accSamples[axisIndex][X] += accADC[X];
accSamples[axisIndex][Y] += accADC[Y];
accSamples[axisIndex][Z] += accADC[Z];
if (isOnFinalAccelerationCalibrationCycle()) {
calibratedAxis[axisIndex] = true;
@ -447,9 +449,9 @@ static void performAcclerationCalibration(void)
static void applyAccelerationZero(const flightDynamicsTrims_t * accZero, const flightDynamicsTrims_t * accGain)
{
acc.accADC[X] = (acc.accADC[X] - accZero->raw[X]) * accGain->raw[X] / 4096;
acc.accADC[Y] = (acc.accADC[Y] - accZero->raw[Y]) * accGain->raw[Y] / 4096;
acc.accADC[Z] = (acc.accADC[Z] - accZero->raw[Z]) * accGain->raw[Z] / 4096;
accADC[X] = (accADC[X] - accZero->raw[X]) * accGain->raw[X] / 4096;
accADC[Y] = (accADC[Y] - accZero->raw[Y]) * accGain->raw[Y] / 4096;
accADC[Z] = (accADC[Z] - accZero->raw[Z]) * accGain->raw[Z] / 4096;
}
void accUpdate(void)
@ -459,30 +461,31 @@ void accUpdate(void)
}
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
acc.accADC[axis] = acc.dev.ADCRaw[axis];
accADC[axis] = acc.dev.ADCRaw[axis];
}
if (!accIsCalibrationComplete()) {
performAcclerationCalibration();
return;
}
applyAccelerationZero(&accelerometerConfig()->accZero, &accelerometerConfig()->accGain);
alignSensors(accADC, acc.dev.accAlign);
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
acc.accADCf[axis] = accADC[axis] / acc.dev.acc_1G;
}
if (accelerometerConfig()->acc_lpf_hz) {
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
acc.accADC[axis] = lrintf(biquadFilterApply(&accFilter[axis], (float)acc.accADC[axis]));
acc.accADCf[axis] = biquadFilterApply(&accFilter[axis], acc.accADCf[axis]);
}
}
#ifdef USE_ACC_NOTCH
if (accelerometerConfig()->acc_notch_hz) {
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
acc.accADC[axis] = lrintf(accNotchFilterApplyFn(accNotchFilter[axis], (float)acc.accADC[axis]));
acc.accADCf[axis] = accNotchFilterApplyFn(accNotchFilter[axis], acc.accADCf[axis]);
}
}
#endif
if (!accIsCalibrationComplete()) {
performAcclerationCalibration();
}
applyAccelerationZero(&accelerometerConfig()->accZero, &accelerometerConfig()->accGain);
alignSensors(acc.accADC, acc.dev.accAlign);
}
void accSetCalibrationValues(void)