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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    Title :

    Disturbance Compensation Based Piecewise Linear Control Design for Perching Maneuvers


    Contributors:
    He, Zhen (author) / Li, Da (author) / Lu, Yuping (author)


    Publication date :

    2019-02-01


    Size :

    766164 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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