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作者机构:Budapest Univ Technol & Econ Dept Measurement & Informat Syst Magyar Tudosok Korutja 2 H-1521 Budapest Hungary
出 版 物:《JOURNAL OF ADVANCED COMPUTATIONAL INTELLIGENCE AND INTELLIGENT INFORMATICS》 (J. Adv. Comput. Intell. Intelligent Informatics)
年 卷 期:2008年第12卷第2期
页 面:198-205页
核心收录:
学科分类:08[工学] 0812[工学-计算机科学与技术(可授工学、理学学位)]
基 金:Hungarian Fund for Scientific Research [OTKA T049519] Structural Fund for Supporting Innovation in Knowledge and Technology Intensive Micro- and Spin-off Enterprises [GVOP-3.3.1.-05/1.2005-05-0160/3.0]
主 题:nonlinear control anytime systems multiple models parallel distributed compensation aeroelastic wing section
摘 要:Nowadays in solving control problems the processing is performed typically by model-based computer systems, which contain a representation of our knowledge about the nature and the actual circumstances of the problem in hand. If the nature and/or the actual circumstances change, the corresponding model should also be changed. Anytime techniques are very flexible in this respect and can advantageously be used when the operation should be performed under changing circumstances. In this paper, a nonlinear state dependant control methodology is proposed for anytime use and as an example is applied to globally stabilize a given prototypical aeroelastic wing section via one control surface.