Major mission of Saturn is to serve as launch vehicle for Apollo lunar landing; based on D.F.Lawden's equation, semi-explicit, "iterative" Saturn guidance equations are derived; they were successfully flight tested on Saturn I and analyzed for main Apollo mission and other applications; Saturn guidance hardware; stability and error analysis.


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    Title :

    Iterative guidance law for Saturn


    Additional title:

    IEEE -- Tech Paper


    Contributors:
    Horn, H.J. (author)

    Conference:

    12th IEEE -- East Coast Conference on Aerospace and Navigational Electronics Meeting ; 1965 Control


    Published in:

    Publication date :

    1965


    Size :

    13 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :