Robust H∞ control has been applied to many different complex dynamic systems, including aircraft. However, since a full-order controller design is used in describing the regular robust output feedback, it is difficult to implement the controller in real time due to its high order. In this paper, a linear matrix equality approach is applied to design a robust proportional-integral (PI) controller for the F-16 aircraft. This approach combines advantages of classical and robust control methods. The resulting controller has a simple structure, is easy for real-time implementation, as well as theoretically guarantees closed-loop stability and performance. A robust H∞ output feedback controller is also designed for comparison. Simulation results validate the effectiveness of the robust PI control.


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    Titel :

    Robust proportional-integral control design for F-16 aircraft using a linear matrix inequality approach


    Beteiligte:
    Huang, B. (Autor:in) / Theodore, Z.B. (Autor:in) / Lu, B. (Autor:in)


    Erscheinungsdatum :

    01.08.2016


    Format / Umfang :

    427866 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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