The operational/functional requirements for the new Microwave Landing System (MLS) are examined for STOL operations. The study utilizes a nonlinear six-degree-of-freedom simulation of a De Havilland Buffalo C-8A aircraft and automatic flight control system to assess the MLS/STOL accuracy, coverage, and data rate requirements for the azimuth, DME, primary elevation, and flare elevation functions. The aircraft performance is statistically determined for representative curved flight paths through touchdown. A range of MLS errors and coverages, environmental disturbances, and navigation filtering are investigated. The study indicates that STOL applications do not place any unique requirements on the MLS.


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    Titel :

    Microwave landing system requirements for STOL operations


    Beteiligte:
    Burrous, C. N. (Autor:in) / Brown, S. C. (Autor:in) / Goka, T. (Autor:in) / Park, K. E. (Autor:in)

    Kongress:

    Aircraft Design, Flight Test and Operations Meeting ; 1974 ; Los Angeles, CA


    Erscheinungsdatum :

    1974-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Microwave landing system requirements for STOL operations

    BURROUS, C. / BROWN, S. / GOKA, T. et al. | AIAA | 1974


    Microwave Landing System Requirements for STOL Operations

    Stuart C. Brown / Clifford N. Burrous / Tsuyoshi Goka et al. | AIAA | 1976


    Preliminary assessment of the microwave landing system requirements for STOL operations

    Burrous, C. N. / Brown, S. C. / Goka, T. et al. | NTRS | 1973


    Flight evaluation of the STOL flare and landing during night operations

    Franklin, J. A. / Innis, R. C. / Hardy, G. H. | NTRS | 1981