From 0ab91a6e9374f190c049a5d8ea1319b9b37529c1 Mon Sep 17 00:00:00 2001 From: cnlohr Date: Sun, 15 Apr 2018 17:43:12 -0400 Subject: Move things into attic and update Makefile to do dependnencies. --- attic/dave/kalman_filter.h | 116 +++++++++++++++++++++++++++++++++++++++++++++ 1 file changed, 116 insertions(+) create mode 100644 attic/dave/kalman_filter.h (limited to 'attic/dave/kalman_filter.h') diff --git a/attic/dave/kalman_filter.h b/attic/dave/kalman_filter.h new file mode 100644 index 0000000..6511fac --- /dev/null +++ b/attic/dave/kalman_filter.h @@ -0,0 +1,116 @@ +#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 + -- cgit v1.2.3