| 某系列运载火箭多射向发射姿态控制方案研究 |
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| 引用本文： | 马卫华.某系列运载火箭多射向发射姿态控制方案研究[J].航天控制,2004,22(2):13-15. |
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| 作者姓名： | 马卫华 |
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| 作者单位： | 北京航天自动控制研究所,北京,100854 |
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| 摘 要： | 介绍了某系列运载火箭实现多射向发射的几种方案 ,比较了它们的优缺点。重点对转动平台和由箭载计算机实现的两种方案从姿态控制系统角度进行了阐述
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| 关 键 词： | 运载火箭 姿态控制系统 射向 轨道 |
| 文章编号： | 1006-3242(2004)02-13-04 |
| 修稿时间： | 2002年6月18日 |
Study on Attitude Control Concept for Multi-launching Direction of Launch Vehicle |
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| Ma WeihuaBeijing Aerospace Automatic Control Institute,Beijing.Study on Attitude Control Concept for Multi-launching Direction of Launch Vehicle[J].Aerospace Control,2004,22(2):13-15. |
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| Authors: | Ma WeihuaBeijing Aerospace Automatic Control Institute Beijing |
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| Institution: | Ma WeihuaBeijing Aerospace Automatic Control Institute,Beijing 100854 |
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| Abstract: | In this paper, several attitude control concepts for multi-launching direction of launch vehicle are presented, then their merits and demerits are compared. The emphases are focused on turntable concept and onboard computer concept, especially from the point of view of attitude control system. |
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| Keywords: | Launch vehicle Attitude control system Launching-direction Trajectory |
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