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GPS/VISNAV integrated relative navig

時(shí)間:2023-05-06 17:13:11 航空航天論文 我要投稿
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GPS/VISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying

Abstract:For the improvement of accuracy and better faulttolerant performance, a global position system (GPS)/vision navigation (VISNAV) integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance. 作者: Author: Xiaoliang Wang  Xiaowei Shao  Deren Gong  Dengping Duan 作者單位: Institute of Aerospace Science & Technology, Shanghai Jiaotong University, Shanghai 200240, P. R. China 期 刊: 系統(tǒng)工程與電子技術(shù)(英文版)   EISCI Journal: JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS 年,卷(期): 2011, 22(2) 分類號(hào): V448.2 Keywords: control and navigation    relative navigation    federal Kalman filter    spacecraft formation flying    global position system (GPS)    vision navigation (VISNAV)    機(jī)標(biāo)分類號(hào): V41 V44 機(jī)標(biāo)關(guān)鍵詞: spacecraft formation flying    attitude determination    performance in    integrated system    attitude estimation    Simulation results    navigation system    Kalman filter    total    approach    GPS    better 基金項(xiàng)目:

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