| 卫星姿态控制推力器布局分析 |
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| 引用本文： | 顾朋,王大轶,刘成瑞.卫星姿态控制推力器布局分析[J].空间控制技术与应用,2013(6):23-28. |
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| 作者姓名： | 顾朋 王大轶 刘成瑞 |
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| 作者单位： | [1]北京控制工程研究所,北京100190 [2]空间智能控制技术重点实验室,北京100190 |
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| 基金项目： | 国家自然科学基金资助项目（61203093）. |
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| 摘 要： | 针对卫星姿态控制过程中推力器数目和分布的选取问题,给出了星上常用的4种推力器安装布局,通过相平面控制,给出了各个稚力器的喷气时间,通过对不同布局下系统的控制精度、燃料消耗和可靠性等方面进行分析和比较,给出了推力器布局设计准则.该准则表明系统的可靠性和燃料消耗是推力器布局设计的主要参考依据.
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| 关 键 词： | 布局 喷气时间 燃料消耗 可靠性 |
Analysis on Thrusters Configuration of Satellite Attitude Control |
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| GU Peng,WANG Day,LIU Chengrui.Analysis on Thrusters Configuration of Satellite Attitude Control[J].Aerospace Contrd and Application,2013(6):23-28. |
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| Authors: | GU Peng WANG Day LIU Chengrui |
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| Institution: | 1. Belting Institute of Control Engineering, Beijing 100190, China; 2. Science and Technology on Space Intelligent Control Laboratory, Belting 100190, China) |
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| Abstract: | Aimed at the problem of choosing appropriate amount and suitable arrangement of thrusters for satellite attitude control, four different configurations of thrusters are summarized. Thruster burn time is given under phase-plane control, and the design criterion is proposed with comparing of control accuracy, fuel consumption and reliability under different configurations. This criterion shows that the reliability and fuel consumption are the primary reference in the design of thruster configuration. |
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| Keywords: | configuration burn time fuel consumption reliability |
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