An in-flight check-out and monitoring approach for an optical communication transceiver terminal on-board a communication satellite will be described. Primarily an inter-pretation of available payload input parameter characteristics will be used, which has no detrimental effect on payload's basic function and which requires only a minimum of additional diagnostic hardware. A method to check out the optical payload pointing, acquisition and tracking function without a counter terminal will be described and means to monitor laser output power at telescope level will be outlined.


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    Titel :

    Transceiver In-Flight Checkout System


    Beteiligte:
    Halm, R. (Autor:in) / Spallicci, A. (Autor:in) / Hahne, A. (Autor:in)

    Kongress:

    Optical Systems for Space Applications ; 1987 ; The Hague,Netherlands


    Erschienen in:

    Erscheinungsdatum :

    18.09.1987





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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