| 小卫星编队飞行动力学及其应用 |
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| 引用本文： | 张振民,林来兴.小卫星编队飞行动力学及其应用[J].航天控制,2002,20(3):44-50. |
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| 作者姓名： | 张振民 林来兴 |
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| 作者单位： | 1. 哈尔滨工业大学,哈尔滨,150001
2. 北京控制工程研究所,北京,100080 |
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| 摘 要： | 由若干颗小卫星编队飞行组成一个虚拟卫星 ,其功能相当或超过一颗大卫星。这将为小卫星开拓一个完全崭新的应用领域。文章首先论述编队飞行的概念和应用 ,其次研究轨道动力学。系统地研究编队飞行三种动力学模型 ,最后进行相应数学仿真 ,分析研究各种数学模型的精度和它们的应用场合。
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| 关 键 词： | 编队飞行 动力学 小卫星 |
| 修稿时间： | 2001年12月9日 |
Formation Flying Dynamics of Small Satellites and It's Application |
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| Zhang zhenmin Harbin University of Technology,Harbin Lin Laixing Beijing Institute of Control Engineering,Beijing.Formation Flying Dynamics of Small Satellites and It's Application[J].Aerospace Control,2002,20(3):44-50. |
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| Authors: | Zhang zhenmin Harbin University of Technology Harbin Lin Laixing Beijing Institute of Control Engineering Beijing |
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| Institution: | Zhang zhenmin Harbin University of Technology,Harbin 150001 Lin Laixing Beijing Institute of Control Engineering,Beijing 100080 |
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| Abstract: | Multiple small satellits flying in formation may constitute a "virtual satellite" with the performance the same as or better than a large satellite This paper will open up a new application field for small satellites The formation flying concepts and their application are firstly outlined, then the orbit dynamics of the "virtual satellite" is investigated Three kinds of dynamics models are described, the model accuracies and their application are analyzed through mathematical simulation |
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| Keywords: | Small satellite Formation flying Orbit dynamics |
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