a Nested PID control loop used for multirotor control.

Dependents:   A-Quad

Files at this revision

API Documentation at this revision

Comitter:
KarimAzzouz
Date:
Tue Aug 27 09:32:17 2013 +0000
Commit message:
initial commit

Changed in this revision

PID.cpp Show annotated file Show diff for this revision Revisions of this file
PID.h Show annotated file Show diff for this revision Revisions of this file
diff -r 000000000000 -r 2ac3074cfdb3 PID.cpp
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/PID.cpp	Tue Aug 27 09:32:17 2013 +0000
@@ -0,0 +1,53 @@
+/* Copyright (c) <2013> MIT License
+ *
+ * Permission is hereby granted, free of charge, to any person obtaining a copy of this software 
+ * and associated documentation files (the "Software"), to deal in the Software without restriction, 
+ * including without limitation the rights to use, copy, modify, merge, publish, distribute, 
+ * sublicense, and/or sell copies of the Software, and to permit persons to whom the Software is 
+ * furnished to do so, subject to the following conditions:
+ *
+ * The above copyright notice and this permission notice shall be included in all copies or 
+ * substantial portions of the Software.
+ *
+ * THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, INCLUDING 
+ * BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND 
+ * NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, 
+ * DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM, 
+ * OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE.
+ *
+ * @section DESCRIPTION
+ *
+ * Nested PID for Quadcopter Control
+ *
+ 
+ */
+ 
+#include "PID.h"
+
+PIDClass::PIDClass(float AngleKp,float AngleKi, float RateKp, float RateKd){
+
+        Angle_Kp=AngleKp;
+        Angle_Ki=AngleKi;
+        Rate_Kp=RateKp;
+        Rate_Kd=RateKd;
+}
+
+int PIDClass::update(float Setpoint, float CurrentPosition, float Rate, float dt){
+      
+      AngleError = Setpoint - CurrentPosition;
+      
+      Angle_I +=AngleError*dt;
+      
+      if(Angle_I>100.0f) Angle_I=100.0f;
+      else if(Angle_I<-100.0f) Angle_I= -100.0f;
+      
+      RateError = (AngleError*Angle_Kp)- Rate;
+      
+      Rate_D = (RateError-PreviousError)/dt;
+      
+      Output = (int)((RateError*Rate_Kp) + (Angle_I*Angle_Ki) + (Rate_D*Rate_Kd));
+      
+      PreviousError = RateError;
+      
+      return Output;
+}
\ No newline at end of file
diff -r 000000000000 -r 2ac3074cfdb3 PID.h
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/PID.h	Tue Aug 27 09:32:17 2013 +0000
@@ -0,0 +1,48 @@
+/* Copyright (c) <2013> MIT License
+ *
+ * Permission is hereby granted, free of charge, to any person obtaining a copy of this software 
+ * and associated documentation files (the "Software"), to deal in the Software without restriction, 
+ * including without limitation the rights to use, copy, modify, merge, publish, distribute, 
+ * sublicense, and/or sell copies of the Software, and to permit persons to whom the Software is 
+ * furnished to do so, subject to the following conditions:
+ *
+ * The above copyright notice and this permission notice shall be included in all copies or 
+ * substantial portions of the Software.
+ *
+ * THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS OR IMPLIED, INCLUDING 
+ * BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE AND 
+ * NONINFRINGEMENT. IN NO EVENT SHALL THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, 
+ * DAMAGES OR OTHER LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING FROM, 
+ * OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN THE SOFTWARE.
+ *
+ * @section DESCRIPTION
+ *
+ * Nested PID for Quadcopter Control
+ *
+ 
+ */
+ 
+#ifndef PID_H
+#define PID_H
+
+#include "mbed.h"
+
+class PIDClass
+{
+
+   public:
+   
+   PIDClass(float AngleKp,float AngleKi, float RateKp, float RateKd);
+   
+   int update(float Setpoint, float CurrentPosition, float Rate, float dt);
+   
+   private:
+   
+        float Angle_Kp,Angle_Ki,Rate_Kp,Rate_Kd;
+        float AngleError,RateError;
+        float Angle_I,Rate_D;
+        int Output,WindUp;
+        float PreviousError;
+
+};
+#endif
\ No newline at end of file