| 捆绑型运载火箭姿态控制系统半实物仿真方法 |
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| 引用本文： | 徐庚保.捆绑型运载火箭姿态控制系统半实物仿真方法[J].航天控制,1990(2). |
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| 作者姓名： | 徐庚保 |
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| 作者单位： | 北京航天自动控制研究所 |
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| 摘 要： | 本文介绍了MPSE软件的主要特点,总结了采用银河仿真机对捆绑型运载火箭姿态控制系统进行半实物仿真的方法。
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| 关 键 词： | 仿真 ~+半实物仿真 姿态控制系统 ~+并行计算 |
HARDWARE IN THE LOOP SIMULATION METHOD USED TO SIMULATE AN ATTITUDE CONTROL SYSTEM OF A BINDING TYPE LAUNCH VEHICLE |
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| Xu Gengbao Beijing Aerospace Automatic Control Institute.HARDWARE IN THE LOOP SIMULATION METHOD USED TO SIMULATE AN ATTITUDE CONTROL SYSTEM OF A BINDING TYPE LAUNCH VEHICLE[J].Aerospace Control,1990(2). |
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| Authors: | Xu Gengbao Beijing Aerospace Automatic Control Institute |
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| Institution: | Xu Gengbao Beijing Aerospace Automatic Control Institute |
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| Abstract: | This paper presents some major characteristics of MPSE software. A hardware in the loop simulation method used to simulate an attitude control system of a binding type launch vehicle with YHFI simulation computer is summarized. |
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| Keywords: | Simulation ~+Hardware in the loop simulation Attitude control system ~+Parallel calculation |
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