| 航天器编队飞行轨道构型研究 |
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| 引用本文： | 林来兴,车汝才.航天器编队飞行轨道构型研究[J].航天器工程,2009,18(1):21-29. |
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| 作者姓名： | 林来兴 车汝才 |
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| 作者单位： | 北京控制工程研究所,北京,100190 |
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| 摘 要： | 通过研究航天器编队飞行轨道动力学和推力控制,提出编队飞行轨道构型有自然式、强迫式和混合式三类,并对每类都举例说明若干种典型构型,以及构型如何建造与所需燃料,文章总共提出14种典型轨道构型,这些构型可供今后编队飞行应用参考。
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| 关 键 词： | 航天器 编队飞行 动力学 轨道构型 研究 |
Study on Orbital Configuration for Spacecraft Formation Flying |
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| LIN Laixing,CHE Rucai.Study on Orbital Configuration for Spacecraft Formation Flying[J].Spacecraft Engineering,2009,18(1):21-29. |
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| Authors: | LIN Laixing CHE Rucai |
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| Institution: | Beijing Institute of Control Engineering;Beijing 100190;China |
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| Abstract: | Based on the study of spacecraft formation flying and thrust control,three kinds of orbital configuration for formation flying,natural configuration,enforced configuration and composite configuration,are propounded in detail.Several typical types of configuration in each kind of orbital configuration and configuration construction and fuel consumiption are presented,and 14 types are proposed in this paper.These types of configuration will be sufficient for the demand of formation flying application in the f... |
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| Keywords: | spacecraft formation flying dynamics orbital configuration research |
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