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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    Title :

    Inertial navigation system for manned aircraft


    Additional title:

    Sperry Eng Rev


    Contributors:
    Klemes, M.S. (author) / Ott, W.J. (author)

    Published in:

    Publication date :

    1963


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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