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计算机工程 ›› 2010, Vol. 36 ›› Issue (8): 236-238. doi: 10.3969/j.issn.1000-3428.2010.08.083

• 工程应用技术与实现 • 上一篇    下一篇

可重构的卫星姿控仿真测试系统设计

颜灵伟1,2,3,张善从1,3   

  1. (1. 中国科学院光电研究院,北京 100190;2. 中国科学院研究生院,北京 100049;3. 北京国科环宇空间技术有限公司,北京 100190)
  • 收稿日期:1900-01-01 修回日期:1900-01-01 出版日期:2010-04-20 发布日期:2010-04-20

Design of Reconfigurable Simulation Test System for Satellite Attitude Control

YAN Ling-wei1,2,3, ZHANG Shan-cong1,3   

  1. (1. Academy of Opto-Electronics, Chinese Academy of Sciences, Beijing 100190; 2. Graduate University of Chinese Academy of Sciences, Beijing 100049; 3. Beijing Trans-Universe Space Technology Co., Ltd., Beijing 100190)
  • Received:1900-01-01 Revised:1900-01-01 Online:2010-04-20 Published:2010-04-20

摘要: 对卫星姿控仿真测试系统的设计需求进行分析和整理,设计和实现一种采用CPCI总线、基于分层模块化的可重构的卫星姿控仿真测试系统,该系统完成了在差异较大的2个型号卫星姿控的仿真测试。仿真实验结果表明,该系统具有应用灵活、通用性和扩展性强等特点。

关键词: 卫星姿控, 仿真测试, 模块化

Abstract: This paper analyses and summarizes the general requirement to simulate the attitude control components, designs and realizes a reconfigurable simulation and testing system for satellite attitude control, which use CPCI bus and based on layered modularization. The system completes two distinct types of satellite attitude control simulate and test task. Simulational experiment results show that the system has flexible application, it is general and expansive.

Key words: satellite attitude control, simulation test, modularization

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