A pilot-vehicle-display model is used to study information and display requirements and the effects on system performance and reliability of pilot-induced randomness, wind gusts, configurational changes, etc. A brief description of a control theoretic systems model is given and its use and validity are demonstrated by applying it in a piloted approach to landing situation. The analysis procedure assumes that the vehicle dynamics are represented by linearized equations of motion.


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    Titel :

    Analytic evaluation of display requirements for approach to landing


    Beteiligte:
    Kleinman, D. L. (Autor:in) / Baron, S. (Autor:in)


    Erscheinungsdatum :

    1972-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Analytic evaluation of display requirements for approach to landing

    Kleinman, David L. / Baron, Sheldon | TIBKAT | 1971


    The Landing Requirements

    Swatton, P. J. | Wiley | 2000


    The Landing Requirements

    Swatton, P. J. | Wiley | 2000


    The Landing Signal Officer: Display Requirements for ACLS Recoveries

    A. Harabedian / G. J. Borden / G. R. Kelley | NTIS | 1972


    Information and display requirements for independent landing monitors

    Karmarker, J. S. / Sorensen, J. A. | NTRS | 1976