Analog version of SGN-10 is self-aligning system that provides navigation and guidance data at 2 nautical mph CEP (Circular Error Probability); it also provides outputs of aircraft attitude, present latitude and longitude, and guidance to 2 destinations; system consists of inertial platform, platform electronics unit, analog computer and control and display panel; paper describes SYG-600 gyroscope and SYP-710 inertial platform on which it is mounted.


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    Titel :

    Inertial navigation system for manned aircraft


    Weitere Titelangaben:

    Sperry Eng Rev


    Beteiligte:
    Klemes, M.S. (Autor:in) / Ott, W.J. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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