Advent of very powerful navigation computers makes it possible by using statistical filtering techniques to retrieve more of information contained in navigation measurements; navigation system is developed as information-filtering problem; Kalman optimum linear filter is found to apply to navigation problem if some technique is used to account for possible nongaussian maneuver accelerations; two methods are suggested which greatly reduce amount of computation with minimum degradation in performance of system; details are given for alignment and calibration of inertial platform using statistical filtering.


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    Titel :

    Statistical estimation in inertial navigation systems


    Weitere Titelangaben:

    J Spacecraft and Rockets


    Beteiligte:
    Brock, L.D. (Autor:in) / Schmidt, G.T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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