Article ID Journal Published Year Pages File Type
11020323 Mathematics and Computers in Simulation 2019 13 Pages PDF
Abstract
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)-α-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.
Related Topics
Physical Sciences and Engineering Engineering Control and Systems Engineering
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