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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    Title :

    Space guidance control technique for radio guided ballistic missiles


    Additional title:

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


    Contributors:
    Flora, D.E. (author) / White, R.A. (author)

    Conference:

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



    Publication date :

    1964


    Size :

    14 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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