摘要
本文提出了基于无复位联邦卡尔曼滤波的信息融合算法,建立了惯性/卫星/天文组合导航系统的误差模型,并进行了计算机仿真。仿真结果表明,该算法具有较强的容错性。
On the base of the NR federated kalman filter information fusion algorithm has been proposed and the error model of the INS/GPS/CNS integrated navigation system has been established. The simulation results demonstrate that this algorithm has good performance of fauh-toleranee.
出处
《微计算机信息》
北大核心
2006年第05S期119-121,共3页
Control & Automation
基金
第二炮兵预研项目编号不公开
