| 卫星-惯性-星光最优组合导航系统在航天飞机导航中的应用 |
| |
| 引用本文： | 郑谔.卫星-惯性-星光最优组合导航系统在航天飞机导航中的应用[J].航空学报,1988,10(10):448-453. |
| |
| 作者姓名： | 郑谔 |
| |
| 作者单位： | 西北工业大学 |
| |
| 摘 要： | 文中对航天飞机星光-惯性导航系统进行了简要分析从最优系统组成原理、余度管理方法、系统性能分析等方面研究了卫星-惯性-星光组合导航系统的概念设计。
|
| 关 键 词： | |
| 收稿时间： | 1987-03-09; |
APPLICATION OF GPS-INS-STAR INTEGRATED NAVIGATION SYSTEM IN SPACECRAFT |
| |
| Northwestern Polytechnical University Zheng E.APPLICATION OF GPS-INS-STAR INTEGRATED NAVIGATION SYSTEM IN SPACECRAFT[J].Acta Aeronautica et Astronautica Sinica,1988,10(10):448-453. |
| |
| Authors: | Northwestern Polytechnical University Zheng E |
| |
| Institution: | Northwestern Polytechnical University Zheng E |
| |
| Abstract: | In this paper the soaceeraft stellar-inertial system is briefly reviewed. In order to generate high grade translational and rotational information of the spacecraft, a concept of GPS-INS-STAR optimal integrated navigation system is studied.The problems discussed include system composition, design philosophy ,performance analysis, inertial measurement unit redundancy management techniques and Kalman filter configuration.Computer simulation results show that this approach would lead to an accurate, autonomous, cost-effective and fault-tolerant navigation system. |
| |
| Keywords: | strapdown inortial system star tracker optimal integration |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《航空学报》浏览原始摘要信息 |
| 点击此处可从《航空学报》下载免费的PDF全文 |
