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Języki publikacji
Abstrakty
This article addresses the challenge of integrated switched H2 control with disturbance rejection capabilities for switched systems, particularly when external disturbances are present. A novel anti-disturbance switched H2 control strategy is formulated, leveraging estimated disturbance values. The formulation is given in Linear Matrix Inequalities (LMIs), establishing sufficient conditions to ensure H2 performance while maintaining closed-loop stability. To validate the effectiveness of the proposed methodology, it is applied to a practical aero-engine model. Through simulations, it is demonstrated that the closed-loop aero-engine model exhibits remarkable transient performance even in the face of external disturbances. These results underscore the efficacy of the developed approach in enhancing the robustness and perfor-mance of switched systems subjected to disturbances. The integration of anti-disturbance capabilities within the H2 control framework offers a promising avenue for addressing real-world control challenges, particularly in systems characterized by switching dynamics and external perturbations.
Czasopismo
Rocznik
Tom
Strony
126--135
Opis fizyczny
Bibliogr. 30 poz., rys., wykr.
Twórcy
autor
- Engineering and Natural sciences, Electrical-Electronics Engineering, Uşak University, Uşak, Turkey
autor
- Engineering, Electrical-Electronics Engineering, Artvin Çoruh University, Artvin, Turkey
Bibliografia
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- 7. Li T, Zhang S, Yang H, et al. Robust missile longitudinal autopilot design based on equivalent-input-disturbance and generalized extended state observer approach. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 2016; 229(6): 1025-1042.
- 8. Aboudonia A, Rashad R, El-Badawy A. Composite hierarchical anti-disturbance control of a quadrotor UAV in the presence of matched and mismatched disturbances. Journal of Intelligent & Robotic Systems. 2018; 90(1): 201-216.
- 9. Zengbo L, Yukai Z, JianzhongnQ. Composite anti-disturbance position and attitude control for spacecraft with parametric uncertainty and flexible vibration. Chinese Journal of Aeronautics. 2022; 35(12): 242-252.
- 10. Liu L, Chen M, Li T, et al. Composite Anti-Disturbance Reference Model 𝐿2−𝐿∞ Control for Helicopter Slung Load System. Journal of Intelligent & Robotic Systems. 2021; 102(1): 1-21.
- 11. Cao S, Guo L, Ding Z. Event‐triggered anti‐disturbance attitude control for rigid spacecrafts with multiple disturbances. International Journal of Robust and Nonlinear Control. 2021; 31(2): 344-357.
- 12. Yao X, Wen X. Composite hierarchical hybrid anti-disturbance control for Markovian jump systems with event-triggered disturbance. Sys-tems & Control Letters. 2024;185:105734.
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- 14. Sun H, Liu Y, Jiao T, et al. Distributed extended state observer design and dual-side dynamic event-triggered output feedback anti-disturb-ance control for nonlinear interconnected systems with quantization. Journal of the Franklin Institute. 2024; 106847.
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- 19. Liu F, Chen M, Li T. Resilient 𝐻∞ control for uncertain turbofan linear switched systems with hybrid switching mechanism and disturbance observer. Applied Mathematics and Computation. 2022; 413: 126597.
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Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a6925840-6555-4168-9255-14c517d095de
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