ESE350 project, Spring 2016, University of Pennsylvania

Dependencies:   Adafruit9-DOf Receiver mbed-rtos mbed

Revision:
34:eaea0ae92dfa
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/Kalman.cpp	Sun Apr 24 17:15:20 2016 +0000
@@ -0,0 +1,76 @@
+#include "Kalman.h"
+
+Kalman::Kalman() {
+    /* We will set the variables like so, these can also be tuned by the user */
+    Q_angle = 0.001f;
+    Q_bias = 0.003f;
+    R_measure = 0.03f;
+
+    angle = 0.0f; // Reset the angle
+    bias = 0.0f; // Reset bias
+
+    P[0][0] = 0.0f; // Since we assume that the bias is 0 and we know the starting angle (use setAngle), the error covariance matrix is set like so - see: http://en.wikipedia.org/wiki/Kalman_filter#Example_application.2C_technical
+    P[0][1] = 0.0f;
+    P[1][0] = 0.0f;
+    P[1][1] = 0.0f;
+};
+
+// The angle should be in degrees and the rate should be in degrees per second and the delta time in seconds
+float Kalman::getAngle(float newAngle, float newRate, float dt) {
+    // KasBot V2  -  Kalman filter module - http://www.x-firm.com/?page_id=145
+    // Modified by Kristian Lauszus
+    // See my blog post for more information: http://blog.tkjelectronics.dk/2012/09/a-practical-approach-to-kalman-filter-and-how-to-implement-it
+
+    // Discrete Kalman filter time update equations - Time Update ("Predict")
+    // Update xhat - Project the state ahead
+    /* Step 1 */
+    rate = newRate - bias;
+    angle += dt * rate;
+
+    // Update estimation error covariance - Project the error covariance ahead
+    /* Step 2 */
+    P[0][0] += dt * (dt*P[1][1] - P[0][1] - P[1][0] + Q_angle);
+    P[0][1] -= dt * P[1][1];
+    P[1][0] -= dt * P[1][1];
+    P[1][1] += Q_bias * dt;
+
+    // Discrete Kalman filter measurement update equations - Measurement Update ("Correct")
+    // Calculate Kalman gain - Compute the Kalman gain
+    /* Step 4 */
+    float S = P[0][0] + R_measure; // Estimate error
+    /* Step 5 */
+    float K[2]; // Kalman gain - This is a 2x1 vector
+    K[0] = P[0][0] / S;
+    K[1] = P[1][0] / S;
+
+    // Calculate angle and bias - Update estimate with measurement zk (newAngle)
+    /* Step 3 */
+    float y = newAngle - angle; // Angle difference
+    /* Step 6 */
+    angle += K[0] * y;
+    bias += K[1] * y;
+
+    // Calculate estimation error covariance - Update the error covariance
+    /* Step 7 */
+    float P00_temp = P[0][0];
+    float P01_temp = P[0][1];
+
+    P[0][0] -= K[0] * P00_temp;
+    P[0][1] -= K[0] * P01_temp;
+    P[1][0] -= K[1] * P00_temp;
+    P[1][1] -= K[1] * P01_temp;
+
+    return angle;
+};
+
+void Kalman::setAngle(float angle) { this->angle = angle; }; // Used to set angle, this should be set as the starting angle
+float Kalman::getRate() { return this->rate; }; // Return the unbiased rate
+
+/* These are used to tune the Kalman filter */
+void Kalman::setQangle(float Q_angle) { this->Q_angle = Q_angle; };
+void Kalman::setQbias(float Q_bias) { this->Q_bias = Q_bias; };
+void Kalman::setRmeasure(float R_measure) { this->R_measure = R_measure; };
+
+float Kalman::getQangle() { return this->Q_angle; };
+float Kalman::getQbias() { return this->Q_bias; };
+float Kalman::getRmeasure() { return this->R_measure; };
\ No newline at end of file