Takagi-Sugeno fuzzy model based robust dissipative control for uncertain flexible spacecraft with saturated time-delay input.
In this paper, the problem of robust dissipative control is investigated for uncertain flexible spacecraft based on Takagi-Sugeno (T-S) fuzzy model with saturated time-delay input. Different from most existing strategies, T-S fuzzy approximation approach is used to model the nonlinear dynamics of flexible spacecraft. Simultaneously, the physical constraints of system, like input delay, input saturation, and parameter uncertainties, are also taken care of in the fuzzy model. By employing Lyapunov-Krasovskii method and convex optimization technique, a novel robust controller is proposed to implement rest-to-rest attitude maneuver for flexible spacecraft, and the guaranteed dissipative performance enables the uncertain closed-loop system to reject the influence of elastic vibrations and external disturbances. Finally, an illustrative design example integrated with simulation results are provided to confirm the applicability and merits of the developed control strategy.
Research Institute of Intelligent Control and Systems, Harbin Institute of Technology, Harbin, HeiLongjiang 150001, PR China. Electronic address: shidongxu@hit.edu.cn.
Shidong
S
Xu
Research Institute of Intelligent Control and Systems, Harbin Institute of Technology, Harbin, HeiLongjiang 150001, PR China. Electronic address: guanghuisun@hit.edu.cn.
Guanghui
G
Sun
Research Institute of Intelligent Control and Systems, Harbin Institute of Technology, Harbin, HeiLongjiang 150001, PR China. Electronic address: 1984sunweichao@gmail.com.
Weichao
W
Sun
Convex optimization technique; Flexible spacecraft; Robust dissipative control; Saturated time-delay input; Takagi–Sugeno fuzzy system