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

一体化结构/控制设计的现状及未来
引用本文:马军平.一体化结构/控制设计的现状及未来[J].航空学报,1993,14(12):621-626.
作者姓名:马军平
作者单位:西安86号信箱 西安 710061
摘    要:从实际应用和数学理论的角度,介绍和评述一体化结构/控制设计的方法。对于性能指标即代价函数的公式,以及个别典型的结果进行了讨论。

关 键 词:一体化设计  伺服气动弹性  多级线性分解  
收稿时间:1992-05-18
修稿时间:1993-02-13

INTEGRATED STRUCTURE / CONTROL DESIGN -PRESENT AND FUTURE
Ma Jun-ping.INTEGRATED STRUCTURE / CONTROL DESIGN -PRESENT AND FUTURE[J].Acta Aeronautica et Astronautica Sinica,1993,14(12):621-626.
Authors:Ma Jun-ping
Institution:Box 86 of Xi'an, Xi'an,710061
Abstract:This paper introduces and comments current methodology applied to the field of Inte-grated Structure / Control Design from both a practical viewpoint and a mathematical viewpoint by a review of the published literature. In the literature, the variety of proposed interdisciplinary objective functions and synthesis methods reflects the multi-disciplinary nature of the problem. Approaches to the problem can generally be grouped into three categories: the sequential methods, the simultaneous methods, and multilevel optimization methods. A discussion of the formulation of performance indices or cost function from these methods is presented in this paper, together with typical results. The multilevel optimizaiton techniques have been found to offer a promising technique as opposed to other integrated design methods. Analytical expressions for optimal sensitivity derivatives related to multilevle optimization are outlined and discussed. The strong tendency is for the beneficial integrated design technology to be used in large orbiting space structure and active controlled, high performance aircraft design.
Keywords:integrated design  aeroservoelasticity  multilevel linear decomposition
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