EKF c语言 姿态融合算法
时间: 2023-12-14 18:34:42 浏览: 36
以下是一个使用EKF算法实现姿态融合的C语言示例代码:
```c
#include <stdio.h>
#include <math.h>
#define PI 3.14159265358979323846
// 定义状态向量
typedef struct {
double q0, q1, q2, q3; // 四元数
double wx, wy, wz; // 陀螺仪测量值
} StateVector;
// 定义观测向量
typedef struct {
double mx, my, mz; // 磁力计测量值
double ax, ay, az; // 加速度计测量值
} ObservationVector;
// 定义协方差矩阵
typedef struct {
double p[7][7];
} CovarianceMatrix;
// 定义常量
const double dt = 0.01; // 采样周期
const double Q = 0.1; // 系统噪声协方差
const double R = 0.5; // 观测噪声协方差
// 定义函数
void EKF(StateVector *x, CovarianceMatrix *P, ObservationVector z, double dt);
void quaternion_normalize(StateVector *x);
void quaternion_multiply(StateVector *x, StateVector q);
void quaternion_update(StateVector *x, ObservationVector z);
int main() {
// 初始化状态向量
StateVector x = {1, 0, 0, 0, 0, 0, 0};
// 初始化协方差矩阵
CovarianceMatrix P = {
.p = {
{1, 0, 0, 0, 0, 0, 0},
{0, 1, 0, 0, 0, 0, 0},
{0, 0, 1, 0, 0, 0, 0},
{0, 0, 0, 1, 0, 0, 0},
{0, 0, 0, 0, 1, 0, 0},
{0, 0, 0, 0, 0, 1, 0},
{0, 0, 0, 0, 0, 0, 1}
}
};
// 初始化观测向量
ObservationVector z = {0.1, 0.2, 0.3, 0, 0, 9.8};
// 进行EKF算法
EKF(&x, &P, z, dt);
// 输出结果
printf("q0 = %f, q1 = %f, q2 = %f, q3 = %f\n", x.q0, x.q1, x.q2, x.q3);
printf("wx = %f, wy = %f, wz = %f\n", x.wx, x.wy, x.wz);
// 返回
return 0;
}
// EKF算法
void EKF(StateVector *x, CovarianceMatrix *P, ObservationVector z, double dt) {
// 定义中间变量
StateVector x_pred;
CovarianceMatrix P_pred;
CovarianceMatrix F;
CovarianceMatrix Q;
CovarianceMatrix H;
CovarianceMatrix R;
CovarianceMatrix K;
ObservationVector z_pred;
double y[6];
double S[6][6];
double det_S;
double inv_S[6][6];
double temp[7][6];
// 预测状态
x_pred.q0 = x->q0 + 0.5 * (-x->q1 * x->wx - x->q2 * x->wy - x->q3 * x->wz) * dt;
x_pred.q1 = x->q1 + 0.5 * (x->q0 * x->wx + x->q2 * x->wz - x->q3 * x->wy) * dt;
x_pred.q2 = x->q2 + 0.5 * (x->q0 * x->wy - x->q1 * x->wz + x->q3 * x->wx) * dt;
x_pred.q3 = x->q3 + 0.5 * (x->q0 * x->wz + x->q1 * x->wy - x->q2 * x->wx) * dt;
x_pred.wx = x->wx;
x_pred.wy = x->wy;
x_pred.wz = x->wz;
// 预测协方差
F.p[0][0] = 1;
F.p[0][1] = -0.5 * x->wx * dt;
F.p[0][2] = -0.5 * x->wy * dt;
F.p[0][3] = -0.5 * x->wz * dt;
F.p[0][4] = 0;
F.p[0][5] = 0;
F.p[0][6] = 0;
F.p[1][0] = 0.5 * x->wx * dt;
F.p[1][1] = 1;
F.p[1][2] = 0.5 * x->wz * dt;
F.p[1][3] = -0.5 * x->wy * dt;
F.p[1][4] = 0;
F.p[1][5] = 0;
F.p[1][6] = 0;
F.p[2][0] = 0.5 * x->wy * dt;
F.p[2][1] = -0.5 * x->wz * dt;
F.p[2][2] = 1;
F.p[2][3] = 0.5 * x->wx * dt;
F.p[2][4] = 0;
F.p[2][5] = 0;
F.p[2][6] = 0;
F.p[3][0] = 0.5 * x->wz * dt;
F.p[3][1] = 0.5 * x->wy * dt;
F.p[3][2] = -0.5 * x->wx * dt;
F.p[3][3] = 1;
F.p[3][4] = 0;
F.p[3][5] = 0;
F.p[3][6] = 0;
F.p[4][0] = 0;
F.p[4][1] = 0;
F.p[4][2] = 0;
F.p[4][3] = 0;
F.p[4][4] = 1;
F.p[4][5] = 0;
F.p[4][6] = 0;
F.p[5][0] = 0;
F.p[5][1] = 0;
F.p[5][2] = 0;
F.p[5][3] = 0;
F.p[5][4] = 0;
F.p[5][5] = 1;
F.p[5][6] = 0;
F.p[6][0] = 0;
F.p[6][1] = 0;
F.p[6][2] = 0;
F.p[6][3] = 0;
F.p[6][4] = 0;
F.p[6][5] = 0;
F.p[6][6] = 1;
Q.p[0][0] = Q;
Q.p[1][1] = Q;
Q.p[2][2] = Q;
Q.p[3][3] = Q;
Q.p[4][4] = Q;
Q.p[5][5] = Q;
Q.p[6][6] = Q;
P_pred = *P;
for (int i = 0; i < 7; i++) {
for (int j = 0; j < 7; j++) {
for (int k = 0; k < 7; k++) {
P_pred.p[i][j] += F.p[i][k] * P->p[k][j];
}
}
}
for (int i = 0; i < 7; i++) {
for (int j = 0; j < 7; j++) {
for (int k = 0; k < 7; k++) {
P_pred.p[i][j] += P->p[i][k] * F.p[j][k];
}
}
}
for (int i = 0; i < 7; i++) {
for (int j = 0; j < 7; j++) {
for (int k = 0; k < 7; k++) {
Q.p[i][j] += F.p[i][k] * Q.p[k][j];
}
}
}
for (int i = 0; i < 7; i++) {
for (int j = 0; j < 7; j++) {
for (int k = 0; k < 7; k++) {
Q.p[i][j] += Q.p[i][k] * F.p[j][k];
}
}
}
// 更新状态
quaternion_multiply(&x_pred, *x);
quaternion_normalize(&x_pred);
// 更新协方差
H.p[0][0] = 2 * x->q0;
H.p[0][1] = -2 * x->q3;
H.p[0][2] = 2 * x->q2;
H.p[0][3] = -2 * x->q1;
H.p[0][4] = 0;
H.p[0][5] = 0;
H.p[0][6] = 0;
H.p[1][0] = 2 * x->q1;
H.p[1][1] = 2 * x->q2;
H.p[1][2] = 2 * x->q3;
H.p[1][3] = 2 * x->q0;
H.p[1][4] = 0;
H.p[1][5] = 0;
H.p[1][6] = 0;
H.p[2][0] = -2 * x->q2;
H.p[2][1] = 2 * x->q1;
H.p[2][2] = 2 * x->q0;
H.p[2][3] = 2 * x->q3;
H.p[2][4] = 0;
H.p[2][5] = 0;
H.p[2][6] = 0;
H.p[3][0] = -2 * x->q3;
H.p[3][1] = -2 * x->q0;
H.p[3][2] = 2 * x->q1;
H.p[3][3] = 2 * x->q2;
H.p[3][4] = 0;
H.p[3][5] = 0;
H.p[3][6] = 0;
H.p[4][0] = 0;
H.p[4][1] = 0;
H.p[4][2] = 0;
H.p[4][3] = 0;
H.p[4][4] = 1;
H.p[4][5] = 0;
H.p[4][6] = 0;
H.p[5][0] = 0;
H.p[5][1] = 0;
H.p[5][2] = 0;
H.p[5][3] = 0;
H.p[5][4] = 0;
H.p[5][5] = 1;
H.p[5][6] = 0;
R.p[0][0] = R;
R.p[1][1] = R;
R.p[2][2] = R;
R.p[3][3] = R;
R.p[4][4] = R;
R.p[5][5] = R;
for (int i = 0; i < 6; i++) {
z_pred.mx = 2 * (x_pred.q1 * x_pred.q3 - x_pred.q0 * x_pred.q2);
z_pred.my = 2 * (x_pred.q0 * x_pred.q1 + x_pred.q2 * x_pred.q3);
z_pred.mz = x_pred.q0 * x_pred.q0 - x_pred.q1 * x_pred.q1 - x_pred.q2 * x_pred.q2 + x_pred.q3 * x_pred.q3;
z_pred.ax = 2 * (x_pred.q1 * x_pred.q3 + x_pred.q0 * x_pred.q2);
z_pred.ay = 2 * (x_pred.q0 * x_pred.q1 - x_pred.q2 * x_pred.q3);
z_pred.az = x_pred.q0 * x_pred.q0 + x_pred.q1 * x_pred.q1 - x_pred.q2 * x_pred.q2 - x_pred.q3 * x_pred.q3;
y[i] = z_pred.mx - z.mx;
y[i + 3] = z_pred.my - z.my;
}
for (int i = 0; i < 6; i++) {
for (int j = 0; j < 7; j++) {
temp[j][i