| 新控制技术与第二代航天飞机 |
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| 引用本文： | 张明廉,路精保,冯亚昌.新控制技术与第二代航天飞机[J].航空学报,1988,10(12):542-548. |
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| 作者姓名： | 张明廉 路精保 冯亚昌 |
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| 作者单位： | 北京航空航天大学
(张明廉，路精保)，北京航空航天大学(冯亚昌) |
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| 摘 要： | 本文介绍了美国航天飞机的概貌,并指出第二代航天飞机的主要特征是水平起降,要实现水平起降,除了要解决动力装置这个关键问题外,必须采用新的控制技术。本文着重分析新控制技术在实现第二代航天飞机中所起的关键作用,可大大减轻航天飞机的自重。
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| 收稿时间： | 1987-08-05; |
NEW CONTROL TECHNIQUES AND THE SECOND GENERATION SHUTTLE |
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| Beijing University of Aeronautics and Astronautics Zhang Minglian Lu Jingbao Feng Yachang.NEW CONTROL TECHNIQUES AND THE SECOND GENERATION SHUTTLE[J].Acta Aeronautica et Astronautica Sinica,1988,10(12):542-548. |
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| Authors: | Beijing University of Aeronautics and Astronautics Zhang Minglian Lu Jingbao Feng Yachang |
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| Institution: | Beijing University of Aeronautics and Astronautics Zhang Minglian Lu Jingbao Feng Yachang |
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| Abstract: | A general survey of A.meriean space shuttle is given in this paper.An important fea-ture of the second generation shuttle is horizontal taking-off and landing,Theretore new control techniques must he taken except from overcoming the key difficulty-new power devices.By using the new control techniques in the second generation shuttle, the deadweight of the shuttle can he effectively reduced. |
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| Keywords: | space shuttle active control Integrated control |
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