An analysis method based on simulation in the time and frequency domains is described for analyzing flutter of a missile fin actuator in the presence of nonlinearities. The method is illustrated by applying it to a hydraulic actuator with backlash and to a pneumatic actuator having nonlinear gas dynamics. All the work was done through computer simulation using the higher order language ACSL.


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    Title :

    Nonlinear flutter analysis of a missile fin/actuator


    Additional title:

    Nichtlineare Schwankungsanalyse eines Flugkoerper-Leitwerks/Antriebs


    Contributors:

    Published in:

    Publication date :

    1986


    Size :

    6 Seiten, 20 Bilder, 3 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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