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LP-289 Further clean up of PIDControlDown::UpdateParameters()
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@ -7,7 +7,8 @@
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* @{
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*
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* @file pidcontroldown.h
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* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2015.
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* @author The LibrePilot Project, http://www.librepilot.org Copyright (C) 2016.
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* The OpenPilot Team, http://www.openpilot.org Copyright (C) 2015.
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* @brief Executes PID control for down direction
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*
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* @see The GNU Public License (GPL) Version 3
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@ -90,13 +91,13 @@ void PIDControlDown::Activate()
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void PIDControlDown::UpdateParameters(float kp, float ki, float kd, float beta, float dT, float velocityMax)
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{
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// pid_configure(&PID, kp, ki, kd, ilimit);
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float Td;
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float Ti;
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float Tt;
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float kt;
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float N = 10.0f;
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float Tf;
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float Td; // Derivative time constant
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float Ti; // Integral time constant
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float kt; // Feedback gain for integral windup avoidance
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float N = 10.0f; // N is the factor used to determine the
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// time constant for derivative filtering
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// Why 10? Maybe should be configurable?
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float Tf; // Low pass filter time constant for derivative filtering
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// Define Td, handling zero kp term (for I or ID controller)
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if (kp < 1e-6f) {
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@ -107,19 +108,17 @@ void PIDControlDown::UpdateParameters(float kp, float ki, float kd, float beta,
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// Define Ti, Tt and kt, handling zero ki term (for P or PD controller)
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if (ki < 1e-6f) { // Avoid Ti being infinite
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Ti = 1e6f;
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// Tt antiwindup time constant - we don't need antiwindup with no I term
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Tt = 1e6f;
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kt = 0.0f;
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} else {
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Ti = kp / ki;
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Tt = (Ti + Td) / 2.0f;
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kt = 1.0f / Tt;
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kt = 1.0f / Ti;
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}
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// Define Tf, according to controller type
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if (kd < 1e-6f) {
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// PI Controller or P Controller
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Tf = Ti / N;
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Tf = 0; // Originally this: (Ti / N) - which creates a D term from
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// the integral time constant!
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} else {
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Tf = Td / N;
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}
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