This paper addressed the initial step toward the goal of establishing performance and handling qualities acceptance criteria for realtime rotorcraft simulators through a planned research effort to quantify the system capabilities of 'selective fidelity' simulators. Within this framework the simulator is then classified based on the required task. The simulator is evaluated by separating the various subsystems (visual, motion, etc.) and applying corresponding fidelity constants based on the specific task. This methodology not only provides an assessment technique, but also provides a technique to determine the required levels of subsystem fidelity for a specific task.


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    Titel :

    Methodology Development for Evaluation of Selective-Fidelity Rotorcraft Simulation


    Beteiligte:
    W. D. Lewis (Autor:in) / D. P. Schrage (Autor:in) / J. V. R. Prasad (Autor:in) / D. Wolfe (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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