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火星探测巡航段天文自主导航方法研究

陈晓 尤伟 黄庆龙

深空探测学报2016,Vol.3Issue(3):214-218,5.
深空探测学报2016,Vol.3Issue(3):214-218,5.DOI:10.15982/j.issn.2095-7777.2016.03.003

火星探测巡航段天文自主导航方法研究

Research on Celestial Navigation for Mars Missions during the Interplanetary Cruising

陈晓 1尤伟 2黄庆龙1

作者信息

  • 1. 哈尔滨工业大学,哈尔滨 150001
  • 2. 上海卫星工程研究所,上海 200240
  • 折叠

摘要

Abstract

For the issue of navigation during the interplanetary cruising,a celestial navigation based on the Sun and Planets observation is proposed. According to the position of a probe in solar system,Sun/Earth and Sun/Mars are selected as targets for navigation observing. Respectively,Sun sensor and optics navigation sensor on the probe are used to measure line of sight. The fundamental of the observation schemes is analyzed and the measurement equations are educed in details. The orbit parameters of the probe are estimated in real time by utilizing extended Kalman filter. Finally,the autonomous navigation methods presented are verified by the data of 2020 Mars mission. Simulation result shows that the estimation accuracy of position and velocity can meet the requirements of the interplanetary cruising phase.

关键词

火星探测/自主导航/视线矢量

Key words

Mars exploration/autonomous navigation/line of sight

引用本文复制引用

陈晓,尤伟,黄庆龙..火星探测巡航段天文自主导航方法研究[J].深空探测学报,2016,3(3):214-218,5.

深空探测学报

2096-9287

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