Philosophy and design of set of "explicit guidance equations" used to control ascent trajectory of radio guided ballistic missile; emphasis is on acquainting nonguidance oriented engineer with control of such re-entry parameters as flight path angle, attitude and velocity; although limited to pitch plane, discussed techniques can be applied to yaw plane.


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    Titel :

    Space guidance control technique for radio guided ballistic missiles


    Weitere Titelangaben:

    IEEE -- East Coast Conf Aerospace Navigational Electronics -- Tech Paper


    Beteiligte:
    Flora, D.E. (Autor:in) / White, R.A. (Autor:in)

    Kongress:

    Meeting of 11th IEEE -- East Coast Conference on Aerospace and Navigational Electronics ; 1964 Orbits and trajectories



    Erscheinungsdatum :

    1964


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Inertial Guidance of Ballistic Missiles

    A. Y. Ishlinskii | NTIS | 1971


    Design of Guided Ballistic Missiles

    A. M. Sinyukov / N. I. Morozov | NTIS | 1970



    Guidance of Ballistic Missiles (Chapters 4-5)

    A. M. Zhakov / F. A. Pigulevskii | NTIS | 1967