void KalmanUpdate(float angle_m,float gyro_m) //gyro_m:gyro_measure { static const float Q_angle=0.001, Q_gyro=0.003, R_angle=300, dt=0.005; //注意:dt的取值为kalman滤波器采样时间; static float P[2][2] = {{ 1, 0 },{ 0, 1 }}; static float Pdot[4] ={0,0,0,0}; static const char C_0 = 1; static float q_bias, angle_err, PCt_0, PCt_1, E, K_0, K_1, t_0, t_1; //------------------------------------------------------- CarAngle+=(gyro_m-q_bias) * dt; Pdot[0] = Q_angle - P[0][1] - P[1][0]; Pdot[1] = -P[1][1]; Pdot[2] = -P[1][1]; Pdot[3] = Q_gyro; P[0][0] += Pdot[0] * dt; 不是应该 P[0][0] += Q_angle -P[0][1]dt - P[1][0]dt-P[1][1]dt*dt 吗? P[0][1] += Pdot[1] * dt; P[1][0] += Pdot[2] * dt; P[1][1] += Pdot[3] * dt; 不是应该 P[1][1] += Pdot[3];吗? angle_err = angle_m - CarAngle; PCt_0 = C_0 * P[0][0]; PCt_1 = C_0 * P[1][0]; E = R_angle + C_0 * PCt_0; K_0 = PCt_0 / E; K_1 = PCt_1 / E; t_0 = PCt_0; t_1 = C_0 * P[0][1]; P[0][0] -= K_0 * t_0; P[0][1] -= K_0 * t_1; P[1][0] -= K_1 * t_0; P[1][1] -= K_1 * t_1; CarAngle += K_0 * angle_err; q_bias += K_1 * angle_err; CarGyro = gyro_m-q_bias; } 求解答。
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