静止轨道自旋卫星离轨控制策略的研究 |
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引用本文: | 袁勇,;李全军,;张瑛,;陈雅容.静止轨道自旋卫星离轨控制策略的研究[J].飞行器测控学报,2008(5):73-76. |
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作者姓名: | 袁勇 ;李全军 ;张瑛 ;陈雅容 |
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作者单位: | [1]西安卫星测控中心,陕西西安710043; [2]空军工程大学,陕西西安710077 |
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摘 要: | 对静止轨道自旋卫星离轨控制策略进行了分析。通过某静止卫星离轨控制的实际工作,分析了有关离轨控制策略制定原则,详细阐述离轨控制策略制定及离轨控制过程中需要考虑的约束条件,总结出适于静止轨道自旋卫星的离轨控制策略。
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关 键 词: | 离轨 控制策略 剩余燃料 |
Research on De-orbiting Control Strategies of Dual-spin Geostationary Orbit Satellites |
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Institution: | YUAN Yong LI Quan-jun ZHANG Ying CHEN Ya-rong (1. Xi'an Satellite Control Center, Xi'an, Shaanxi Province 710043; 2. Air Force Engineering University, Xi'an, Shaanxi Province 710077) |
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Abstract: | This paper analyzes the de-orbiting control strategies of dual-spin geostationary orbit satellites. Based on de-orbiting control operations of a GEO satellite, principles for drawing up de-orbiting control strategies are described. Constraints to be taken into consideration for de-orbiting control are discussed. Finally, de-orbiting control strategies for dual-spin geostationary orbit satellites are given. |
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Keywords: | De-orbiting Control Strategies Surplus Fuel |
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