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。
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.
出处
《航天控制》
CSCD
北大核心
2004年第1期42-45,共4页
Aerospace Control