This paper will discuss the airborne flight test of the Sikorsky UH-60 Black Hawk helicopter in turbulent conditions to determine disturbance rejection criteria and develop a low speed wind/turbulence model for helicopter simulation.


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    Title :

    UH-60 Black Hawk Disturbance Rejection Study for Hover/Low Speed Handling Qualities Criteria and Turbulence Modeling


    Contributors:

    Publication date :

    1999-01-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English