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-rw-r--r--dave/kalman_filter.h116
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diff --git a/dave/kalman_filter.h b/dave/kalman_filter.h
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--- a/dave/kalman_filter.h
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-#ifndef __KALMAN_FILTER_H__
-#define __KALMAN_FILTER_H__
-
-#include "dclapack.h"
-
-/* * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * *
- * Legend:
- * xhat_k_km1 -- Predicted state at time 'k' using information available at time 'k-1'
- * P_k_km1 -- Predicted covariance at time 'k' using information available at time 'k-1'
- * F_k -- State transition model
- * u_k -- Control vector (i.e. external process)
- * B_k -- Control input model
- * w_k -- Gaussian White noise
- * H_k -- Observation model (to transform true state into measurements)
- * Q_k -- Covariance matrix of process noise
- * R_k -- Covariance of observational noise
- * v_k -- Gaussian white observational noise
- *
- * PREDICTION PHASE
- * Predicted state: xhat_k_km1 = Fk * xhat_km1_km1 + Bk * uk
- * Predicted covar: P_k_km1 = Fk * P_km1_km1 * Fk' + Qk
- *
- * UPDATE PHASE
- * Measurement residual: yhat_k = zk - Hk * xhat_k_km1
- * Residual covariance: S_k = H_k * P_k_km1 * H_k' + R_k
- * Optimal Kalman gain: K_k = P_k_km1 * H_k' * inv(S_k)
- * Updated state esti: xhat_k_k = xhat_k_km1 + K_k * yhat_k
- * Updated covariance: P_k_k = (I - K_k * H_k) * P_k_km1
- * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * */
-
-#define KAL_STRIDE 36
-#define KAL_MAT(_var) float _var[ORDER][ORDER]
-#define KAL_VEC(_var) float _var[ORDER][ORDER]
-
-void KalmanPredict(
- KAL_VEC(xhat_k_km1), /* OUTPUT: (S) Predicted state at time 'k' */
- KAL_MAT(P_k_km1), /* OUTPUT: (S x S) Predicted covariance at time 'k' */
- KAL_MAT(P_km1_km1), /* INPUT: (S x S) Updated covariance from time 'k-1' */
- KAL_VEC(xhat_km1_km1), /* INPUT: (S) Updated state from time 'k-1' */
- KAL_MAT(F_k), /* INPUT: (S x S) State transition model */
- KAL_MAT(B_k), /* INPUT: (S x U) Control input model */
- KAL_VEC(u_k), /* INPUT: (U) Control vector */
- KAL_MAT(Q_k), /* INPUT: (S x S) Covariance of process noise */
- int S, /* INPUT: Number of dimensions in state vector */
- int U); /* INPUT: Size of control input vector */
-
-void KalmanUpdate(
- KAL_VEC(xhat_k_k), /* (S) OUTPUT: Updated state at time 'k' */
- KAL_MAT(P_k_k), /* (S x S) OUTPUT: Updated covariance at time 'k' */
- KAL_VEC(xhat_k_km1), /* (S) INPUT: Predicted state at time 'k' */
- KAL_MAT(P_k_km1), /* (S x S) INPUT: Predicted covariance at time 'k' */
- KAL_VEC(z_k), /* (B) INPUT: Observation vector */
- KAL_MAT(H_k), /* (B x S) INPUT: Observational model */
- KAL_MAT(R_k), /* (S x S) INPUT: Covariance of observational noise */
- int B, /* INPUT: Number of observations in observation vector */
- int S); /* INPUT: Number of measurements in the state vector */
-
-/* * * * * * * * * * * *
- * State vector format:
- * xhat[12] = { x, y, z, ix, iy, iz, jx, jy, jz, kx, ky, kz, vx, vy, vz, vix, viy, viz, vjx, vjy, vjz, vkx, vky, vkz, ax, ay, az, aix, aiy, aiz, ajx, ajy, ajz, akx, aky, akz },
- * 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35
- * where,
- * i -- right direction vector
- * j -- forward direction vector
- * k -- up direction vector
- * * * * * * * * * * * */
-
-/* positional state */
-#define ST_X 0
-#define ST_Y 1
-#define ST_Z 2
-#define ST_IX 3
-#define ST_IY 4
-#define ST_IZ 5
-#define ST_JX 6
-#define ST_JY 7
-#define ST_JZ 8
-#define ST_KX 9
-#define ST_KY 10
-#define ST_KZ 11
-
-/* velocity state */
-#define ST_VX 12
-#define ST_VY 13
-#define ST_VZ 14
-#define ST_VIX 15
-#define ST_VIY 16
-#define ST_VIZ 17
-#define ST_VJX 18
-#define ST_VJY 19
-#define ST_VJZ 20
-#define ST_VKX 21
-#define ST_VKY 22
-#define ST_VKZ 23
-
-/* acceleration state */
-#define ST_AX 24
-#define ST_AY 25
-#define ST_AZ 26
-#define ST_AIX 27
-#define ST_AIY 28
-#define ST_AIZ 29
-#define ST_AJX 30
-#define ST_AJY 31
-#define ST_AJZ 32
-#define ST_AKX 33
-#define ST_AKY 34
-#define ST_AKZ 35
-
-
-/* * * * * * * * * * * *
- * Measurement:
- * * * * * * * * * * * */
-
-#endif
-