The patent relates to an apparatus that improves external load modal damping, provides the pilot command control augmentation of the load, and minimizes pilot induced oscillation, and is universally adaptable to a wide variety of helicopters. The apparatus contemplates rigid pendants which damp load motion in response to a sensor.


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    Title :

    External Load Stabilization Apparatus


    Contributors:
    J. H. Smith (author)

    Publication date :

    1974


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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