Robust flight control system design using <i>H</i>_∞ loop-shaping and recessive trait crossover genetic algorithm

作     者：El-Mahallawy, A. A. Yousef, H. A. El-Singaby, M. I. Madkour, A. A. Youssef, A. M. 

作者机构：Sultan Qaboos Univ Dept Elect & Comp Engn Muscat 123 Oman Mil Tech Coll Cairo 11787 Egypt Arab Acad Sci & Technol Coll Engn & Technol Alexandria Egypt 

出 版 物：《EXPERT SYSTEMS WITH APPLICATIONS》 (专家系统及其应用)

年 卷 期：2011年第38卷第1期

页      面：169-174页

核心收录：

学科分类：1201[管理学-管理科学与工程(可授管理学、工学学位)] 0808[工学-电气工程] 08[工学] 0812[工学-计算机科学与技术（可授工学、理学学位）] 

主　　题：Recessive trait crossover genetic algorithm H-infinity loop-shaping Flight simulations Control augmentation system 

摘      要：A proposed approach to robust controller design is introduced. This approach combines the recessive trait crossover genetic algorithm with the loop-shaping design procedure using H-infinity synthesis. The requirements, design and simulation of a flight control system for precision tracking task are considered. The proposed method is applied to design a control system for the F-16 fighter aircraft model. The flight simulations reveal that the desired performance objectives are achieved and that the controller provides acceptable performance in spite of modeling errors and plant parameter variations. (C) 2010 Elsevier Ltd. All rights reserved.