The methodology of simulation application in the design process of a helicopter is discussed. The simulation facility is described and the main features of the simulation model are explained. Special emphasis is laid on engine, landing gear, noise, and vibration modeling. The validation of the model was performed by use of trim values, time histories, derivatives, and frequency responses. A mission analysis is discussed using the example of an EMS mission. Exemplary investigations for the evaluation of mission effectiveness, control response behavior, and system failures are covered.


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    Titel :

    Mission Oriented Investigation of Handling Qualities through Simulation


    Beteiligte:
    D. Braun (Autor:in) / K. Kampa (Autor:in) / D. Schimke (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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