Dynamics and control, stability, and guidance analyses are summarized for the asymmetrical booster ascent guidance and control system design studies, performed in conjunction with space shuttle planning. The mathematical models developed for use in rigid body and flexible body versions of the NASA JSC space shuttle functional simulator are briefly discussed, along with information on the following: (1) space shuttle stability analysis using equations of motion for both pitch and lateral axes; (2) the computer program used to obtain stability margin; and (3) the guidance equations developed for the space shuttle powered flight phases.


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    Title :

    Asymmetrical booster ascent guidance and control system design study. Volume 1: Summary


    Contributors:

    Publication date :

    1974-06-28


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :