An iterative method is described for determining the impulses and the times of the impulses which are needed to effect a prescribed orbit change for the case where the propulsion system orientation is given. The method makes use of an existing computer program and is demonstrated by two examples.


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    Title :

    Stationkeeping of Geostationary Satellites Zur Positionshaltung Geostationaerer Satelliten


    Contributors:

    Publication date :

    1976


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English