A linear error covariance analysis is performed for a satellite borne stellar horizon atmospheric dispersion (SHAD) sensor for the purpose of evaluating its feasibility for autonomous satellite orbit determination. The unmodeled errors of the Earth atmosphere limit the sensor's ultimate precision as a navigational instrument. Although less measurement precision is required for low satellite altitudes, the atmospheric effects are more severe. In order to achieve positional accuracies of less than 200 meters, atmospheric errors need to be limited to 1 % or less. This paper is condensed version of a paper previously given at the AAS/AIAA Astrodynamics Conference, Lake Placid, New York, Aug. 22-25, 1983.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Autonomous satellite navigation using the stellar horizon atmospheric dispersion sensor


    Weitere Titelangaben:

    Autonome Satellitennavigation mit dem atmosphaerischen Sternenhorizont Dispersions-Sensor (SHAD)


    Beteiligte:
    Liu, A.S. (Autor:in)


    Erscheinungsdatum :

    1986


    Format / Umfang :

    6 Seiten, 6 Bilder, 4 Tabellen, 2 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Autonomous satellite navigation by stellar refraction

    GOUNLEY, R. / WHITE, R. / GAI, E. | AIAA | 1983


    Autonomous satellite navigation by stellar refraction

    Gounley, R. / White, R. / Gai, E. | NTRS | 1984


    Autonomous satellite navigation by stellar refraction

    GOUNLEY, R. / Charles Stark Draper Laboratory / Inc. et al. | AIAA | 1984


    Autonomous over-the-horizon navigation using LIDAR data

    Rekleitis, I. | British Library Online Contents | 2013


    Celestial Navigation Method of a Satellite using Star Tracker and Horizon Sensor

    MOON KYU JIN / RYOO CHANG KYUNG / PARK WOO SUNG et al. | Europäisches Patentamt | 2017

    Freier Zugriff