THE simplest concept of inertial navigation is that of using an accelerometcr for measurement of vehicle acceleration, integrating once to give a measure of velocity and twice to give a measure of distance travelled (fig. 1). For this purpose, the direction of the input axis of the accelerometcr must be kept constant, or alternatively its direction at all times must be known and its changing direction must be taken into account in interpreting its output. In either case, provision of a stable attitude reference is necessary. Gyroscopes can provide this feature.


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    Titel :

    Aircraft Inertial Navigation


    Untertitel :

    A Description of Gyroscopes and Accelerometers suitable for Navigational Purposes, the Principles Involved in Inertial Navigation round the Earth and the Combination of Doppler and Inertial Systems


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


    Erscheinungsdatum :

    01.01.1964


    Format / Umfang :

    8 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Aircraft inertial navigation

    Lee, J.A. | Engineering Index Backfile | 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