In order to improve the ability of satellite’s autonomic survivorship,this thesis aims at low earth orbit satellite, studies on integrated navigation system consists of the strap-down inertial navigation system(SINS)、the land-based navigation system and celestial navigation system(CNS).
为了提高卫星自主生存的能力,本课题针对低轨道卫星,研究了捷联惯导系统(SINS)、陆基导航系统以及星敏感器(CNS)的组合导航系统。
参考来源 - 基于SINS/陆基/星敏感器的组合导航研究·2,447,543篇论文数据,部分数据来源于NoteExpress
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