首页 | 本学科首页   官方微博 | 高级检索  
     检索      


New general guidance method in constrained optimal control,part 2: Application to space shuttle guidance
Authors:B Kugelmann  H J Pesch
Institution:(1) Department of Mathematics, University of Technology, Munich, Germany;(2) Faculty of Computer Science, University of the Armed Forces, Munich, Germany
Abstract:The application and the performance of the neighboring optimal feedback scheme presented in Part 1 of this paper is demonstrated for the heating-constrained cross-range maximization problem of a space-shuttle-orbiter-type vehicle. This problem contains five state variables, two control variables, and a state variable inequality constraint of order zero.This research was supported in part by the Deutsche Forschungsgemeinschaft under the Schwerpunktprogramm ldquoAnwendungsbezogene Optimierung und Steuerung.rdquoThe authors wish to express their sincere and grateful appreciation to Professor Roland Bulirsch who encouraged this work.
Keywords:Neighboring extremals  accessory minimum problem  feedback controls  neighboring optimum guidance  multiple shooting  guidance of space vehicles  space shuttle
本文献已被 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号