Adaptive Guidance Mode system under development at Marshall Space Flight Center must be sufficiently broad to accommodate variety of vehicle configurations and missions; guidance and control system consists of four-gimbal inertial platform system with necessary items for maximum flexibility and unlimited attitude freedom, computing system capable of meeting requirements for all foreseeable missions, and analog control system that orients and stabilizes vehicle.


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    Title :

    Saturn ascending phase guidance and control techniques


    Additional title:

    Progress Astronautics Aeronautics


    Contributors:
    Moore, F.B. (author) / Brooks, M. (author)


    Publication date :

    1963


    Size :

    27 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Saturn Ascending Phase Guidance and Control Techniques

    Cummings, Clifford I. / Lawrence, Harold R. | AIAA | 1963


    SATURN ASCENDING PHASE GUIDANCE AND CONTROL TECHNIQUES

    Brooks, M. / Moore, F. B. | NTRS | 1963


    Saturn guidance concepts

    Baker, C. D. | NTRS | 1967


    Saturn guidance concepts

    Baker, C. D. | NTRS | 1965