Description of gyroscopes and accelerometers suitable for navigational purposes; principles involved in inertial navigation round earth are explained; it is shown that pure inertial system is undamped, that introduction of damping leads to system errors, but that these can be eliminated by use of velocity measurement from Doppler system; advantages of combination of Doppler and inertial systems; comparison of individual and combined systems.


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    Titel :

    Aircraft inertial navigation


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Lee, J.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aircraft Inertial Navigation

    Lee, J.A. | Emerald Group Publishing | 1964


    Inertial navigation system for manned aircraft

    Klemes, M.S. / Ott, W.J. | Engineering Index Backfile | 1963




    Doppler-inertial navigation for high performance aircraft

    Reel, L.S. | Engineering Index Backfile | 1959