This paper investigates the control design approach for perching maneuvers of fixed-wing aircraft in the presence of both initial deviations and mismatched disturbances. The highly nonlinear longitudinal dynamics is transformed into a piecewise linear model. A disturbance observer is designed and a piecewise linear controller using the estimates of disturbances is constructed. System stability and disturbance attenuation are analyzed theoretically. Simulation results demonstrate the effectiveness of the proposed control approach.


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    Titel :

    Disturbance Compensation Based Piecewise Linear Control Design for Perching Maneuvers


    Beteiligte:
    He, Zhen (Autor:in) / Li, Da (Autor:in) / Lu, Yuping (Autor:in)


    Erscheinungsdatum :

    01.02.2019


    Format / Umfang :

    766164 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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