Comparative evaluation of translunar injection accuracies achievable with various updating procedures and state-of-art inertial guidance systems; techniques for computing performance errors due to error sources associated with guidance hardware are presented; estimation theory is applied, using radar tracking as independent source of measurement to improve estimate of vehicle performance; comparison of translunar injection precision, attainable by updating on parking orbit, is made using ideal estimation, estimation at each tracking station, and recursive estimation; numerical results are presented.


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    Titel :

    Error analysis of navigation using inertial guidance and radar tracking


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Remmler, K.L. (Autor:in) / Theobald, R.T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :