This paper examines a switching Linear Parameter-Varying (LPV) control approach to determine if it is practical to use for flight control designs within a wide angle of attack region. The approach is based on multiple parameter-dependent Lyapunov functions. The full parameter space is partitioned into overlapping subspaces and a family of LPV controllers are designed, each suitable for a specific parameter subspace. The hysteresis switching logic is used to accomplish the transition among different parameter subspaces. The proposed switching LPV control scheme is applied to an F-16 aircraft model with different actuator dynamics in low and high angle of attack regions. The nonlinear simulation results show that the aircraft performs well when switching among different angle of attack regions.


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    Titel :

    Switching LPV Control for High Performance Tactical Aircraft


    Beteiligte:
    Lu, Bei (Autor:in) / Wu, Fen (Autor:in) / Kim, SungWan (Autor:in)

    Kongress:

    AIAA Guidance, Navigation and Control Conference ; 2004 ; Providence, RI, United States


    Erscheinungsdatum :

    01.01.2004


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch





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