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Changed rate controller from PID to PIDT1 to improve flight stability.
Low pass on D-Term makes the D-Term usable to improve flight stability. Affects rate and stabilize mode.
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@ -68,6 +68,7 @@ typedef struct {
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float iLim;
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float iLim;
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float iAccumulator;
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float iAccumulator;
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float lastErr;
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float lastErr;
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float lastDer;
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} pid_type;
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} pid_type;
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// Private variables
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// Private variables
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@ -405,6 +406,7 @@ static void stabilizationTask(void* parameters)
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float ApplyPid(pid_type * pid, const float err, float dT)
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float ApplyPid(pid_type * pid, const float err, float dT)
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{
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{
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float diff = (err - pid->lastErr);
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float diff = (err - pid->lastErr);
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float dterm = 0;
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pid->lastErr = err;
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pid->lastErr = err;
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// Scale up accumulator by 1000 while computing to avoid losing precision
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// Scale up accumulator by 1000 while computing to avoid losing precision
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@ -414,7 +416,16 @@ float ApplyPid(pid_type * pid, const float err, float dT)
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} else if (pid->iAccumulator < -(pid->iLim * 1000.0f)) {
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} else if (pid->iAccumulator < -(pid->iLim * 1000.0f)) {
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pid->iAccumulator = -pid->iLim * 1000.0f;
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pid->iAccumulator = -pid->iLim * 1000.0f;
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}
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}
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return ((err * pid->p) + pid->iAccumulator / 1000.0f + (diff * pid->d / dT));
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// Calculate DT1 term, fixed T1 timeconstant
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if(pid->d)
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{
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dterm = pid->lastDer + (( dT / ( dT + 7.9577e-3)) * ((diff * pid->d / dT) - pid->lastDer));
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pid->lastDer = dterm; // ^ set constant to 1/(2*pi*f_cutoff)
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// 7.9577e-3 means 20 Hz f_cutoff
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}
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return ((err * pid->p) + pid->iAccumulator / 1000.0f + dterm);
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}
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}
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@ -423,6 +434,7 @@ static void ZeroPids(void)
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for(int8_t ct = 0; ct < PID_MAX; ct++) {
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for(int8_t ct = 0; ct < PID_MAX; ct++) {
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pids[ct].iAccumulator = 0.0f;
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pids[ct].iAccumulator = 0.0f;
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pids[ct].lastErr = 0.0f;
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pids[ct].lastErr = 0.0f;
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pids[ct].lastDer = 0.0f;
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}
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}
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for(uint8_t i = 0; i < 3; i++)
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for(uint8_t i = 0; i < 3; i++)
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axis_lock_accum[i] = 0.0f;
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axis_lock_accum[i] = 0.0f;
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