A nonlinear simulation model of the CH-47B helicopter was adapted for use in the NASA Ames Research Center (ARC) simulation facility. The model represents the specific configuration of the ARC variable stability CH-47B helicopter and will be used in ground simulation research and to expedite and verify flight experiment design. Modeling of the helicopter uses a total force approach in six rigid body degrees of freedom. Rotor dynamics are simulated using the Wheatlely-Bailey equations including steady-state flapping dynamics. Also included in the model is the option for simulation of external suspension, slung-load equations of motion.


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    Titel :

    Mathematical Simulation Model of the CH-47B Helicopter, Volume 1


    Beteiligte:
    J. M. Weber (Autor:in) / T. Y. Liu (Autor:in) / W. Chung (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    137 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    A mathematical simulation model of the CH-47B helicopter, volume 1

    Weber, J. M. / Liu, T. Y. / Chung, W. | NTRS | 1984



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    Leontiv, V. A. / Anikin, V. A. / American Helicopter Society | British Library Conference Proceedings | 2002


    A Mathematical Simulation of Integrated Helicopter Avionics

    Murphy, James P. / Pickens, DeWitt H. | IEEE | 1966