The objective of this program was to develop, design, and flight test a roll-axis Hydrofluidic Stability Augmentation System (HYSAS) for the OH-58A helicopter. The system, when used with a yaw HYSAS, provides increased vehicle damping which improves the handling characteristics. Flight test evaluations were performed with satisfactory results.


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    Title :

    Roll-Axis Hydrofluidic Stability Augmentation System Development


    Contributors:
    D. Bengtson (author) / T. Dickovich (author) / R. Helfenstine (author)

    Publication date :

    1975


    Size :

    137 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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