A satellite tracking system and method, a three-point peaking technique is used to determine the direction of a satellite 50 which includes a signal source. A Kalman filter is used to minimize the effects of noise in the received signal during the three-point peaking operation. This determination may be made at any time. Once the position of a satellite 50 has been determined twice over a time interval, its future position may be estimated by an adaptive continuous step track technique, using a Kalman filter, which assumes that the satellite moves uniformly with time as viewed from the antenna.


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    Titel :

    TRACK HIGHLY INCLINED SATELLITES WITH NOISE AFFECTED SIGNALS


    Weitere Titelangaben:

    HOCH GENEIGTE SATELLITEN MIT BAHN UND VON GERÄUSCHEN BETROFFENEN SIGNALEN
    POURSUITE DE SATELLITES FORTEMENT INCLINÉS AVEC DES SIGNAUX AFFECTÉS PAR LE BRUIT


    Beteiligte:

    Erscheinungsdatum :

    04.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS