24 hr satellite and navigational satellite system are discussed with respect to guidance requirements during launch, orbit transfer, final orbit injection and in-orbit correction; parametric data are presented in graphical form and numerical values given for sample problems; also discussed are selection of navigational satellite pattern, and determination of space vehicle position by use of navigational satellite system.


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    Titel :

    Satellite vehicle guidance requirements


    Weitere Titelangaben:

    IRE Nat Symp Space Electronics Telemetry -- Trans


    Beteiligte:
    Jensen, J. (Autor:in) / Townsend, G. (Autor:in)

    Kongress:

    5th IRE National Symposium on Space Electronics and Telemetry ; 1960 Control



    Erscheinungsdatum :

    1960


    Format / Umfang :

    23 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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