Aircraft navigation using doppler and orbital information transmitted from a satellite is shown to be feasible, at least in a limited sense. The least squares, differential correction method of computation is used. If sufficiently accurate velocity information can be provided, this approach could yield positions for long-range aircraft that are an order of magnitude more accurate than have been achieved with other world-wide, all-weather, all-altitude systems, such as doppler and inertial navigators. The least squares, differential corrections solutions for both position and velocity do not converge for reasonable initial errors. Therefore, accurate aircraft velocity components, such as those provided by a doppler navigator, must be known. For one knot velocity errors the position of a 500-knot aircraft can be determined to one-half nautical mile or better for latitudes up to 70 degrees. (Author)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft Navigation by Satellite


    Beteiligte:
    H. A. Myers (Autor:in)

    Erscheinungsdatum :

    1962


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Satellite Navigation and Communication Systems: Aircraft Integration

    Grossin, J. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1994


    Status and future of aircraft satellite navigation

    Weihe, I. | Engineering Index Backfile | 1968



    Satellite Navigation and Communication Systems: Aircraft Integration

    Grossin, J. | British Library Online Contents | 1994


    AIRCRAFT NAVIGATION EFFICIENCY IMPROVING DURING LANDING USING SATELLITE NAVIGATION SYSTEM

    Volodymyr Kharchenko / Valeriy Konin / Tetiana Olevinska | DOAJ | 2017

    Freier Zugriff