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

考虑一阶环节和法向约束的最优导引律
引用本文:詹致祥.考虑一阶环节和法向约束的最优导引律[J].航空学报,1986,7(3):291-297.
作者姓名:詹致祥
作者单位:西北工业大学
摘    要:前言 目前关于最优导引律的文献中,除文献讨论了将导引对象视为具有瞬时响应特性的质点,考虑了控制的法向约束而外,其他均未考虑控制的约束问题。为了大幅度地提高导引精度,在建立“导引对象--目标”的数学模型时,就必须考虑导引对象的动态响应。

关 键 词:
收稿时间:1984-11-09;

OPTIMAL GUIDANCE LAW WITH FIRST ORDER LAG LOOP AND NORMAL CONSTRAINT
Zhan Zhixiang.OPTIMAL GUIDANCE LAW WITH FIRST ORDER LAG LOOP AND NORMAL CONSTRAINT[J].Acta Aeronautica et Astronautica Sinica,1986,7(3):291-297.
Authors:Zhan Zhixiang
Institution:Northwestern Polytechnical University
Abstract:An optimal guidance law based on the maximum principle is discussed in this paper. It is assumed that the kinetic characteristics of "vehicle-target"are that of a first order lag loop which can be described as follows:the performance index is the minimum control energy consumptionthe terminal states belong to a intecept curved surface with control cutoff and the terminal acceleration of the vehicle equals zero:the control force satisfies the normal constraint:Based on these assumptions, an analytical form of the closed loop optimal intercept guidance law has been deduced.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
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