Star tracking systems evolved for long range missiles; initial stages in development; advantages and disadvantages; tracking mechanism; sun tracking missiles; it is concluded that maximum range of missile may be limited, not by its tracking ability, but by response of its radio receivers to weak signal at extreme distances before lock can be opened. See also Engineering Index 1951 p 743.


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    Title :

    Celestial guidance for missiles


    Additional title:

    Aero Digest


    Contributors:

    Published in:

    Aero Digest ; 64 , n 1


    Publication date :

    1952


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Guidance -- Brains of missiles

    Sigley, D.T. / Korman, N.I. / Worsley, G. | Engineering Index Backfile | 1956


    Neoclassical Guidance for Homing Missiles

    Pini Gurfil / Mario Jodorkovsky / Moshe Guelman | AIAA | 2001


    Nonlinear clos guidance for missiles

    Aggarwal, R.K. / Moore, C.R. | Tema Archive | 1985


    Guidance concepts for tactical missiles

    Sorensen, O.C. | Engineering Index Backfile | 1964


    Inertial Guidance of Ballistic Missiles

    A. Y. Ishlinskii | NTIS | 1971