摘要
结合 INS/GPS组合导航系统 ,讨论了卡尔曼滤波直接法的应用。仿真结果证明
This paper discussed the application of Kalman direct filtering in INS/GPS integrated navigation systerm.The systerm equqtion of Kalman filter is provided,the algorithms for linearity is discussed. Computer simulation results show that the use of Kalman direct filtering can improve the accuracy of integrated navigation systerm efficiently.
出处
《弹箭与制导学报》
CSCD
北大核心
2002年第1期28-30,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
国防预研基金资助
