Information Sciences: an International Journal
Multiobjective control for T-S fuzzy singularly perturbed systems
IEEE Transactions on Fuzzy Systems
H∞ control for fuzzy singularly perturbed systems
Fuzzy Sets and Systems
Design of Output Feedback Controller for Attitude Control System of Flexible Satellite Based on LMI
WNIS '09 Proceedings of the 2009 International Conference on Wireless Networks and Information Systems
Robust H∞ control for a class of discrete time fuzzy systems via delta operator approach
Information Sciences: an International Journal
Information Sciences: an International Journal
H∞ filtering for fuzzy singularly perturbed systems with pole placement constraints: an LMI approach
IEEE Transactions on Signal Processing
Filtering for Fuzzy Singularly Perturbed Systems
IEEE Transactions on Systems, Man, and Cybernetics, Part B: Cybernetics
IEEE Transactions on Systems, Man, and Cybernetics, Part B: Cybernetics
IEEE Transactions on Fuzzy Systems
Stability analysis and synthesis of fuzzy singularly perturbed systems
IEEE Transactions on Fuzzy Systems
IEEE Transactions on Fuzzy Systems
Control Synthesis of Singularly Perturbed Fuzzy Systems
IEEE Transactions on Fuzzy Systems
Technical Communique: Effects of small delays on stability of singularly perturbed systems
Automatica (Journal of IFAC)
Universal fuzzy controllers based on generalized T--S fuzzy models
Fuzzy Sets and Systems
Robust stability of impulsive Takagi-Sugeno fuzzy systems with parametric uncertainties
Information Sciences: an International Journal
IEEE Transactions on Systems, Man, and Cybernetics, Part B: Cybernetics
Information Sciences: an International Journal
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This paper investigates the problems of modeling and controller design for complex flexible nonlinear systems (CFNSs) based on a fuzzy singularly perturbed model. A standard discrete-time fuzzy singularly perturbed model (FSPM) is firstly constructed to estimate CFNSs. Based on a matrix spectral norm approach, a static output feedback controller is designed, which guarantees the resulting closed-loop system is asymptotically stable. The gains of controllers are obtained by solving a set of @e-independent linear matrix inequalities (LMIs) so the ill-conditioned problems caused by @e can be easily avoided. Finally, the proposed approach is applied to modeling and attitude control of flexible satellites. In contrast to the existing results, the proposed method has the following advantages: (i) flexible vibrations can be effectively suppressed, and (ii) the control performance is greatly improved, as well as (iii) the control inputs do not need to be limited in controller design. Two practical examples are provided to illustrate the effectiveness of the presented approach. From the simulation results, it can be seen that the proposed approach can also effectively overcome the external disturbances and noises.