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| 大型捆绑运载火箭姿态控制系统 | |
| 引用本文： | 杨德生.大型捆绑运载火箭姿态控制系统[J].航天控制,1991(1). |
| 作者姓名： | 杨德生 |
| 作者单位： | 北京航天自动控制研究所 |
| 摘 要： | 本文介绍了大型捆绑运载火箭姿态控制系统方案、工作原理和首发飞行试验结果,并将部分参数同美国航天飞机进行比较。 |
| 关 键 词： | 姿态控制系统 ~+姿态角速度控制回路 ~+质心控制回路 人工智能 航天飞机 |
ATTITUDE CONTROL SYSTEM OF A LARGE-SCALE STRAP-ON LAUNCH VEHICLE |
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| Yang Deshong Beijing Aerospace Automatic Control Institute.ATTITUDE CONTROL SYSTEM OF A LARGE-SCALE STRAP-ON LAUNCH VEHICLE[J].Aerospace Control,1991(1). | |
| Authors: | Yang Deshong Beijing Aerospace Automatic Control Institute |
| Institution: | Yang Deshong Beijing Aerospace Automatic Control Institute |
| Abstract: | This paper introduces in detail the scheme and principle of the attitude control system of a large-scale launch vehicle in which four boosters are strapped-on and flight test results. A part of parameters of system are compared with that of the Americal Space Shuttle. |
| Keywords: | Attitude control system ~+Attitude angle rate control loop ~+Mass center Artificial intelligence Space shuttle |
| 本文献已被 CNKI 等数据库收录！ | |