NAOC Open IR
组合大视场星敏感器星光折射卫星自主导航方法及仿真
金声震1; 孙才红1; 宁书年2; 王国权2
2005
Source Publication系统仿真学报
ISSN1004-731X
Volume017Issue:003Pages:529
Abstract通过分析影响星光折射法卫星自主导航精度的因素,给出一种高精度自主导航的新方法。即利用组合大视场星敏感器,同时观测整个地球边缘的三颗恒星,通过卫星、地球、恒星方向之间的位置关系及给出的星光大气折射模型,精确确定地心方位,实现高精度自主导航。结合推广的卡尔曼滤波算法,建立了该方法的仿真模型,以某地球同步卫星为背景,利用模拟数据进行了系统仿真。仿真结果表明,该新方法具有较高的导航精度。
Language英语
Document Type期刊论文
Identifierhttp://ir.bao.ac.cn/handle/114a11/51514
Collection中国科学院国家天文台
Affiliation1.中国科学院国家天文台
2.中国矿业大学
First Author AffilicationNational Astronomical Observatories, Chinese Academy of Sciences
Recommended Citation
GB/T 7714
金声震,孙才红,宁书年,等. 组合大视场星敏感器星光折射卫星自主导航方法及仿真[J]. 系统仿真学报,2005,017(003):529.
APA 金声震,孙才红,宁书年,&王国权.(2005).组合大视场星敏感器星光折射卫星自主导航方法及仿真.系统仿真学报,017(003),529.
MLA 金声震,et al."组合大视场星敏感器星光折射卫星自主导航方法及仿真".系统仿真学报 017.003(2005):529.
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