Delayed sub-optimal control for active flutter suppression of a three-dimensional wing

被引:7
|
作者
Zhou, Qing [1 ]
Yu, Zhangwei [1 ]
Cai, Guoping [1 ]
机构
[1] Shanghai Jiao Tong Univ, State Key Lab Ocean Engn, Dept Engn Mech, Shanghai 200240, Peoples R China
基金
上海市自然科学基金;
关键词
Flexible wing; Flutter; Sub-optimal control; Time delay; Second-order sensitivity; FAULT-TOLERANT CONTROL; STATE-FEEDBACK; TIME-DELAY; DESIGN;
D O I
10.1016/j.jfluidstructs.2018.03.009
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, delayed sub-optimal control based on partial-state feedback for flutter suppression system involving time-delay is investigated, and the effectiveness of the suboptimal controller is compared with the optimal controller based on full-state feedback, Firstly, the aeroservoelastic (ASE) model of the flexible wing with control surfaces is given, and the method to dispose the time-delay in the control input is introduced. Then, the determination of the importance of each state in control feedback is studied using the second-order sensitivity of the performance index with respect to the control gain. Finally, the effectiveness of sub-optimal controller is compared with optimal controller through numerical simulations. Simulation results show that the importance of states can be effectively determined by the second-order sensitivity, and the delayed sub-optimal controller can achieve a control effect quite close to the delayed optimal controller. The order of the delayed suboptimal controller designed in this paper is lower, so it shows more engineering significance. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:275 / 287
页数:13
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