The report describes efforts leading to the determination of minimum suitable scan rates for the azimuth and Elevation functions of the microwave Landing Guidance System (LGS) proposed by RTCA SC-117, based on performance requirements of two conventionally equipped civilian aircraft. Two complementary methods are used; one involving a full nonlinear digital simulation, the other involving direct covariance matrix propagation. Wind and turbulence models, aircraft models and LGS models are described in detail. (Author)


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    Titel :

    An Investigation of Microwave Landing Guidance System Signal Requirements for Conventionally Equipped Civilian Aircraft


    Beteiligte:
    M. H. Lanman (Autor:in)

    Erscheinungsdatum :

    1971


    Format / Umfang :

    189 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch