Dissipative analysis for aircraft flight control systems with randomly occurring uncertainties via non-fragile sampled-data control

被引:20
作者
Kumar, S. Vimal [1 ]
Anthoni, S. Marshal [2 ]
Raja, R. [3 ]
机构
[1] RVS Tech Campus Coimbatore, Dept Math, Coimbatore 641402, Tamil Nadu, India
[2] Anna Univ, Dept Math, Reg Campus, Coimbatore 641046, Tamil Nadu, India
[3] Alagappa Univ, Ramanujan Ctr Higher Math, Karaikkudi 630004, Tamil Nadu, India
关键词
Flight control systems; Dissipative; Non-fragile sampled-data control; Randomly occurring uncertainties; TIME-VARYING DELAY; NEURAL-NETWORKS; STABILITY ANALYSIS; ACTUATOR FAILURES; LEAKAGE DELAYS; DESIGN;
D O I
10.1016/j.matcom.2018.03.009
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This work investigates the problem of robust dissipative analysis for aircraft flight control systems via non-fragile sampled-data control approach. The uncertainties occurring in the system parameter is assumed to be random and satisfy the Bernoulli distribution. The main objective of this work is to design a non-fragile sampled-data controller such that the resulting closed-loop system is robustly stochastically stable and strictly (Q, S, R)-alpha-dissipative. By constructing a suitable augmented Lyapunov-Krasovskii functional (LKF) with Lyapunov stability theory, some sufficient conditions are composed in the structure of linear matrix inequalities (LMIs) and it can be interpreted through some known software collection. Finally, a practical example with simulation is provided to indicate the usefulness of the suggested control design technique. (C) 2018 International Association for Mathematics and Computers in Simulation (IMACS). Published by Elsevier B.V. All rights reserved.
引用
收藏
页码:217 / 226
页数:10
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