System offers passive method of orbit determination and yet maintains parameters relative to earth or lunar reference points; it provides vehicle attitude, position and velocity by onboard calculations using measurements taken by on-board instrumentation; such systems have no buildup of instrument error with time and do not depend on ground tracking support to maintain high accuracy and control of its own trajectory parameters; computer simulation programs determine magnitudes of net errors obtained from given navigation system; discrepancies between predicted and actual measurements are given filter factors and added to actual measurements to produce best estimate of vehicle position and velocity.


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    Titel :

    Laser electro-optical navigation system


    Weitere Titelangaben:

    IEEE -- Nat Aerospace Electronics Conference -- Proc


    Beteiligte:
    Williams, R.M. (Autor:in)

    Kongress:

    Proceedings of the 17th IEEE National Aerospace Electronics Conference ; 1965 Electronic equipment



    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Electro-Optical Navigation for Aircraft

    Menon, P.K.A. | Online Contents | 1993


    Electro-optical navigation for aircraft

    Menon, P. K. A. / Chatterji, Gano B. / Sridhar, Banavar | NTRS | 1993



    PERFORMANCE OF INTEGRATED ELECTRO-OPTICAL NAVIGATION SYSTEMS

    Hoshizaki, T. / Andrisani, D. / Braun, A. W. et al. | British Library Online Contents | 2004