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RDSS/INS紧组合及在无源RDSS导航系统中的应用
引用本文:王永刚,王顺宏.RDSS/INS紧组合及在无源RDSS导航系统中的应用[J].航天控制,2004,22(1):42-45.
作者姓名:王永刚  王顺宏
作者单位:北京航空航天大学,北京,100083;第二炮兵工程学院,西安,710025
摘    要:基于RDSS双星导航定位系统可靠性分析 ,提出了利用RDSS/INS紧密组合实现RDSS无源连续导航的方案 ,并针对RDSS/INS几种组合方案进行了初步仿真分析。仿真结果表明 :利用RDSS/INS紧密组合可在中低动态用户中实现高精度无源连续RDSS导航。

关 键 词:RDSS  组合制导  可靠性
文章编号:1006-3242(2004)01-42-04
修稿时间:2003年7月9日

RDSS/INS Tight Combination and Its Application in Realizing the No-source RDSS Navigation
Wang Yonggang,Wang Shunhong.RDSS/INS Tight Combination and Its Application in Realizing the No-source RDSS Navigation[J].Aerospace Control,2004,22(1):42-45.
Authors:Wang Yonggang  Wang Shunhong
Institution:Wang Yonggang +1 Wang Shunhong +21. Beijing University of Aeronautics and Astronautics,Beijing 100083 2. The Second Artillery Engineering College,Xi'an 710025
Abstract:On the basis of analysis of reliability about RDSS, RDSS/INS tightly integrated Navigation system is put forward in the is paper so as to realize no-source navigation of RDSS ; some elementary simulations are taken and the results show RDSS/INS tight integration can effectively realize the no-source RDSS navigation for medium and low dynamic user.
Keywords:RDSS Combined guidance Reliability  
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