Description of self-contained aids which fall into two groups, air data and Doppler radar; inertial navigation combines constant direction-seeking properties of gyroscope with accelerometers and integrators to provide navigation system with six major characteristics which are described; operational uses of inertial navigation systems and use of combined Doppler inertial systems are examined together with overall system aspects of complete navigation system. Article is based on paper presented before IATA Aircraft Navigation Conference, Miami, Fla 1965.


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    Titel :

    Performance of inertial navigation equipment


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Roberts, G.E. (Autor:in) / Treadgold, M.G. (Autor:in)

    Erschienen in:

    Flight ; 89 , n 2971


    Erscheinungsdatum :

    1966


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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