NAOC Open IR
卫星自主定轨中轨道摄动仿真
薛申芳1; 孙才红2; 宁书年1; 金声震2
2004
Source Publication系统仿真学报
ISSN1004-731X
Volume016Issue:007Pages:1395
Abstract针对组合大视场星敏感器卫星自主定轨方法,建立了地球非球形摄动下的广义卡尔曼滤波仿真模型,滤波过程采用了新的改进算法。通过计算机仿真,说明该自主定轨方法具有很高的位置、速度均方误差估计精度且算法是收敛的。计算给出了一日内的卫星轨道,反映了在地球非球形摄动下轨道的变化情况,且对轨道面的进动进行了计算。
Language英语
Document Type期刊论文
Identifierhttp://ir.bao.ac.cn/handle/114a11/42600
Collection中国科学院国家天文台
Affiliation1.中国矿业大学
2.中国科学院国家天文台
Recommended Citation
GB/T 7714
薛申芳,孙才红,宁书年,等. 卫星自主定轨中轨道摄动仿真[J]. 系统仿真学报,2004,016(007):1395.
APA 薛申芳,孙才红,宁书年,&金声震.(2004).卫星自主定轨中轨道摄动仿真.系统仿真学报,016(007),1395.
MLA 薛申芳,et al."卫星自主定轨中轨道摄动仿真".系统仿真学报 016.007(2004):1395.
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