| 航天器的模块化姿态控制系统 |
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| 引用本文： | 陈祖贵. 航天器的模块化姿态控制系统[J]. 航天控制, 1992, 0(1) |
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| 作者姓名： | 陈祖贵 |
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| 作者单位： | 北京控制工程研究所 |
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| 摘 要： | 本文首先介绍航天器模块化姿态控制系统的基本概念和发展概况。接着介绍模块化姿态系统的构成及其主要部件,并以陆地卫星—4(Landsat—D)为例介绍模块化姿态控制系统的应用。最后对发展我国模块化姿态控制系统提出某些建议和设想,以供参考。
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| 关 键 词： | 航天器 姿态控制系统 ~*模块化 |
Spacecraft Modular Attitude Control System(MACS) |
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| Chen Zugui Beijing Institute of Control Engineering. Spacecraft Modular Attitude Control System(MACS)[J]. Aerospace Control, 1992, 0(1) |
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| Authors: | Chen Zugui Beijing Institute of Control Engineering |
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| Affiliation: | Chen Zugui Beijing Institute of Control Engineering |
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| Abstract: | In this paper, basic concept and development summary of spacecraft MACS is presented first; then the constitution of MACS and its main components; and the landsat-D is taken as an example to illustrate the applieation of MACS; finally some proposals for developing the MACS in our country are given a reference. |
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| Keywords: | Subject terms Spaceeraft Attitude control system Modulzarijation |
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