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Code Issues Wiki Activity

Switch Control Derivative to PT2 filter

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Pawel Spychalski (DzikuVx) 2021-06-26 14:30:48 +02:00
parent 92bc8364ce
commit e0860d1fa8
1 changed files with 3 additions and 3 deletions
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6
src/main/flight/pid.c
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@ -110,7 +110,7 @@ typedef struct {
bool itermLimitActive;
bool itermFreezeActive;
biquadFilter_t rateTargetFilter;
pt2Filter_t rateTargetFilter;
smithPredictor_t smithPredictor;
} pidState_t;
@ -356,7 +356,7 @@ bool pidInitFilters(void)
if (pidProfile()->controlDerivativeLpfHz) {
for (int axis = 0; axis < XYZ_AXIS_COUNT; axis++) {
biquadFilterInitLPF(&pidState[axis].rateTargetFilter, pidProfile()->controlDerivativeLpfHz, getLooptime());
pt2FilterInit(&pidState[axis].rateTargetFilter, pt2FilterGain(pidProfile()->controlDerivativeLpfHz, refreshRate * 1e-6f));
}
}
@ -816,7 +816,7 @@ static void FAST_CODE NOINLINE pidApplyMulticopterRateController(pidState_t *pid
const float newDTerm = dTermProcess(pidState, dT);
const float rateTargetDelta = pidState->rateTarget - pidState->previousRateTarget;
const float rateTargetDeltaFiltered = biquadFilterApply(&pidState->rateTargetFilter, rateTargetDelta);
const float rateTargetDeltaFiltered = pt2FilterApply(&pidState->rateTargetFilter, rateTargetDelta);
/*
* Compute Control Derivative