The present invention relates to a satellite constellation realization method for implementing communication by utilizing a recursive orbit. The method comprises following steps: determining a regression period and a semi-major axis of an orbit, as well as an inclination, an eccentricity and an argument of perigee of the orbit; determining both the number of satellites and the number of orbital planes as n ; determining right ascension of a ascending node and a mean anomaly of a first satellite, and sequentially determining right ascension of ascending nodes and mean anomalies of subsequent satellites according to satellite service requirements; determining a set of geostationary orbit satellite networks that need to be coordinated, and a width of a guard band for interference of a non-geostationary satellite constellation on a geostationary satellite; at any location on the ground, all deployed satellites can be seen passing overhead successively along a fixed and identical trajectory in the air, and a user at ground can simultaneously see multiple satellites when multi-coverage is formed; if a satellite trajectory crosses the guard band for interference on the geostationary satellite, then when a currently-accessed satellite enters the guard band, the user at ground switching to another satellite not in the guard band to continue to implement communication.


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    Title :

    SATELLITE CONSTELLATION IMPLEMENTATION METHOD FOR PERFORMING COMMUNICATION BY USING REGRESSION ORBIT


    Additional title:

    IMPLEMENTIERUNGSVERFAHREN FÜR SATELLITENKONSTELLATION ZUR DURCHFÜHRUNG EINER KOMMUNIKATION MITTELS REGRESSIONSUMLAUFBAHN
    PROCÉDÉ DE MISE EN OEUVRE D'UNE CONSTELLATION DE SATELLITES SERVANT À RÉALISER UNE COMMUNICATION AU MOYEN D'UNE ORBITE DE RÉGRESSION


    Contributors:
    JIN JIN (author) / YAN JIAN (author) / KUANG LINLING (author)

    Publication date :

    2019-09-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H04B TRANSMISSION , Übertragung / B64G Raumfahrt , COSMONAUTICS