mirror of
https://github.com/betaflight/betaflight.git
synced 2025-07-18 05:45:31 +03:00
Add acc and gyro accumulators to improve attitude estimation
This commit is contained in:
parent
d3d5b107cc
commit
22c672fa7d
9 changed files with 79 additions and 14 deletions
|
@ -69,6 +69,10 @@
|
|||
|
||||
acc_t acc; // acc access functions
|
||||
|
||||
static float accumulator[XYZ_AXIS_COUNT];
|
||||
static timeUs_t accumulatedTimeUs;
|
||||
static timeUs_t lastTimeSampledUs;
|
||||
|
||||
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.
|
||||
|
||||
extern uint16_t InflightcalibratingA;
|
||||
|
@ -463,7 +467,7 @@ static void applyAccelerationTrims(const flightDynamicsTrims_t *accelerationTrim
|
|||
acc.accSmooth[Z] -= accelerationTrims->raw[Z];
|
||||
}
|
||||
|
||||
void accUpdate(rollAndPitchTrims_t *rollAndPitchTrims)
|
||||
void accUpdate(timeUs_t currentTimeUs, rollAndPitchTrims_t *rollAndPitchTrims)
|
||||
{
|
||||
if (!acc.dev.readFn(&acc.dev)) {
|
||||
return;
|
||||
|
@ -492,6 +496,32 @@ void accUpdate(rollAndPitchTrims_t *rollAndPitchTrims)
|
|||
}
|
||||
|
||||
applyAccelerationTrims(accelerationTrims);
|
||||
|
||||
const timeDelta_t sampleDeltaUs = currentTimeUs - lastTimeSampledUs;
|
||||
lastTimeSampledUs = currentTimeUs;
|
||||
accumulatedTimeUs += sampleDeltaUs;
|
||||
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
|
||||
accumulator[axis] += acc.accSmooth[axis] * sampleDeltaUs;
|
||||
}
|
||||
}
|
||||
|
||||
bool accGetAccumulationAverage(float *accumulation)
|
||||
{
|
||||
if (accumulatedTimeUs > 0) {
|
||||
const float accumulatedTimeS = accumulatedTimeUs * 1e-6;
|
||||
// If we have gyro data accumulated, calculate average rate that will yield the same rotation
|
||||
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
|
||||
accumulation[axis] = accumulator[axis] / accumulatedTimeS;
|
||||
accumulator[axis] = 0.0f;
|
||||
}
|
||||
accumulatedTimeUs = 0;
|
||||
return true;
|
||||
} else {
|
||||
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
|
||||
accumulation[axis] = 0.0f;
|
||||
}
|
||||
return false;
|
||||
}
|
||||
}
|
||||
|
||||
void setAccelerationTrims(flightDynamicsTrims_t *accelerationTrimsToUse)
|
||||
|
|
Loading…
Add table
Add a link
Reference in a new issue