The proposed research will examine the use of an integrated controller for the primary flight control of a helicopter. The primary controls of pitch, roll, and yaw will be integrated into a single, side-stick controller. Two types of integrated controllers will be studied: 1) an isotonic (displacement) controller; and 2) an isometric (force) controller. The two integrated control configurations will be compared to the conventional arrangement via performance on a 3-axis compensatory tracking task. RMS error will provide the dependent measure. (Author)


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    Titel :

    Helicopter Integrated Controller Research


    Beteiligte:
    S. L. Dunbar (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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