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https://github.com/ArduPilot/ardupilot
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uncrustify libraries/AP_PID/AP_PID.cpp
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@ -14,52 +14,52 @@ AP_PID::AP_PID()
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long
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AP_PID::get_pid(int32_t error, uint16_t dt, float scaler)
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{
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float output = 0;
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float delta_time = (float)dt / 1000.0;
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float output = 0;
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float delta_time = (float)dt / 1000.0;
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// Compute proportional component
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output += error * _kp;
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// Compute proportional component
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output += error * _kp;
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// Compute derivative component if time has elapsed
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if ((fabs(_kd) > 0) && (dt > 0)) {
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float derivative = (error - _last_error) / delta_time;
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// Compute derivative component if time has elapsed
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if ((fabs(_kd) > 0) && (dt > 0)) {
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float derivative = (error - _last_error) / delta_time;
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// discrete low pass filter, cuts out the
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// high frequency noise that can drive the controller crazy
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float RC = 1/(2*M_PI*_fCut);
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derivative = _last_derivative +
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(delta_time / (RC + delta_time)) * (derivative - _last_derivative);
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// discrete low pass filter, cuts out the
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// high frequency noise that can drive the controller crazy
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float RC = 1/(2*M_PI*_fCut);
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derivative = _last_derivative +
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(delta_time / (RC + delta_time)) * (derivative - _last_derivative);
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// update state
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_last_error = error;
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_last_derivative = derivative;
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// update state
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_last_error = error;
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_last_derivative = derivative;
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// add in derivative component
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output += _kd * derivative;
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}
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// add in derivative component
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output += _kd * derivative;
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}
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// scale the P and D components
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output *= scaler;
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// scale the P and D components
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output *= scaler;
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// Compute integral component if time has elapsed
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if ((fabs(_ki) > 0) && (dt > 0)) {
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_integrator += (error * _ki) * scaler * delta_time;
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if (_integrator < -_imax) {
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_integrator = -_imax;
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} else if (_integrator > _imax) {
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_integrator = _imax;
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}
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output += _integrator;
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}
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// Compute integral component if time has elapsed
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if ((fabs(_ki) > 0) && (dt > 0)) {
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_integrator += (error * _ki) * scaler * delta_time;
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if (_integrator < -_imax) {
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_integrator = -_imax;
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} else if (_integrator > _imax) {
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_integrator = _imax;
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}
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output += _integrator;
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}
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return output;
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return output;
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}
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void
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AP_PID::reset_I()
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{
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_integrator = 0;
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_last_error = 0;
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_last_derivative = 0;
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_integrator = 0;
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_last_error = 0;
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_last_derivative = 0;
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}
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