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- W2200321179 abstract "In this brief, a fast robust integrated guidance and control design approach, considering the 3-D interception of interceptors for hypersonic vehicles, is proposed. The proposed method is designed using the modified fast terminal sliding mode control and dynamic surface control with signal compensation. The fractional integral fast terminal sliding functions are presented independently, and all the sliding phases run parallel to increase the system response speed. Utilizing the dynamic surface control method, the robust compensation signals are constructed to eliminate the influence of uncertainty equivalents thoroughly. Therefore, the proposed approach guarantees the fast convergence of line-of-sight angular rates and the system robustness for uncertainties. The simulation results demonstrate the robustness of the proposed controller, and a variety of comparison studies are also carried out to demonstrate the advantage of the new approach." @default.
- W2200321179 created "2016-06-24" @default.
- W2200321179 creator A5023358501 @default.
- W2200321179 creator A5086357154 @default.
- W2200321179 date "2016-01-01" @default.
- W2200321179 modified "2023-10-16" @default.
- W2200321179 title "Fast Robust Integrated Guidance and Control Design of Interceptors" @default.
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- W2200321179 doi "https://doi.org/10.1109/tcst.2015.2431641" @default.
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