A controller for an electrohydraulic active control landing gear was developed for the F-4 aircraft. A controller was modified for this application. Simulation results indicate that during landing and rollout over repaired bomb craters the active gear effects a force reduction, relative to the passive gear, or approximately 70%.


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    Title :

    An electronic control for an electrohydraulic active control landing gear for the F-4 aircraft


    Contributors:
    Ross, I. (author)

    Publication date :

    1982-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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