new
Dependencies: mbed
Diff: kalman.cpp
- Revision:
- 0:77a7d1a1c6db
diff -r 000000000000 -r 77a7d1a1c6db kalman.cpp --- /dev/null Thu Jan 01 00:00:00 1970 +0000 +++ b/kalman.cpp Sat Dec 03 18:21:47 2016 +0000 @@ -0,0 +1,52 @@ +#include "kalman.h" +// derived from http://blog.tkjelectronics.dk/2012/09/a-practical-approach-to-kalman-filter-and-how-to-implement-it/ +kalman::kalman(void){ + P[0][0] = 0; + P[0][1] = 0; + P[1][0] = 0; + P[1][1] = 0; + + angle = 0; + bias = 0; + + Q_angle = 0.001; + Q_gyroBias = 0.003; + R_angle = 0.03; +} + +double kalman::getAngle(double newAngle, double newRate, double dt){ + //predict the angle according to the gyroscope + rate = newRate - bias; + angle = dt * rate; + //update the error covariance + 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] += dt * Q_gyroBias; + //difference between the predicted angle and the accelerometer angle + y = newAngle - angle; + //estimation error + S = P[0][0] + R_angle; + //determine the kalman gain according to the error covariance and the distrust + K[0] = P[0][0]/S; + K[1] = P[1][0]/S; + //adjust the angle according to the kalman gain and the difference with the measurement + angle += K[0] * y; + bias += K[1] * y; + //update the error covariance + P[0][0] -= K[0] * P[0][0]; + P[0][1] -= K[0] * P[0][1]; + P[1][0] -= K[1] * P[0][0]; + P[1][1] -= K[1] * P[0][1]; + + return angle; +} +void kalman::setAngle(double newAngle) { angle = newAngle; }; +void kalman::setQangle(double newQ_angle) { Q_angle = newQ_angle; }; +void kalman::setQgyroBias(double newQ_gyroBias) { Q_gyroBias = newQ_gyroBias; }; +void kalman::setRangle(double newR_angle) { R_angle = newR_angle; }; + +double kalman::getRate(void) { return rate; }; +double kalman::getQangle(void) { return Q_angle; }; +double kalman::getQbias(void) { return Q_gyroBias; }; +double kalman::getRangle(void) { return R_angle; }; \ No newline at end of file