This paper describes a dynamic aircraft hydraulic system simulator model. This model uses a flexible approach that accounts for flight control loads, system stiffness, line losses, internal leakage at individual valve packages, pump compensator response, and power input to engine-driven pumps at various engine rpm. The model integrates performance of the flight controls, hydraulics, and power sources allowing accurate simulation of the airplane.


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    Title :

    Dynamic hydraulic system simulation - An integrated approach


    Additional title:

    Dynamische Simulation eines hydraulischen Systems - Eine integrierte Näherung


    Contributors:
    Bang, B.J. (author) / Draxler, J.G. (author)

    Published in:

    SAE-Papers ; Oct ; 1-10


    Publication date :

    1990


    Size :

    10 Seiten, 4 Bilder



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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