航空学报 > 1988, Vol. 10 Issue (12): 542-548

新控制技术与第二代航天飞机

张明廉, 路精保, 冯亚昌   

  1. 北京航空航天大学
  • 收稿日期:1987-08-05 修回日期:1900-01-01 出版日期:1988-12-25 发布日期:1988-12-25

NEW CONTROL TECHNIQUES AND THE SECOND GENERATION SHUTTLE

Zhang Minglian,Lu Jingbao,Feng Yachang   

  1. Beijing University of Aeronautics and Astronautics
  • Received:1987-08-05 Revised:1900-01-01 Online:1988-12-25 Published:1988-12-25

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。

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.