Hodographs are obtained from analysis of roots of inertial system computer equations for errors in determining coordinates of longitudinal and lateral motion of flight vehicle, which correspond to angular velocity variation over total possible range; qualitative study of inertial-system properties for high speed flight; results obtained for velocity of 8 km/sec are compared with known theory in celestial mechanics. (see also English translation in Eng Cybernetics n 2 Mar-Apr 1965 p 158-69)


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    Title :

    Analysis of inertial systems of navigation for high speed flight


    Additional title:

    Povedenie inertsial'nykh sistem navigatsii pri bol'shikh skorostyakh poleta


    Contributors:


    Publication date :

    1965


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Russian


    Keywords :