Review of basic design parameters which largely determine functional and hardware design of flight control system of any manned spacecraft, namely, vehicle type, mission duration, mission objective, vehicle weight, and method of thermal equipment control; X-20 flight control system for delta-winged orbital glider; Apollo's command module's stabilization and control system (SCS); its control functions and elements; flight control for orbital stations; future control systems.


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    Title :

    Flight control for manned spacecraft


    Additional title:

    Space/Aeronautics


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Balanced-in-flight testing for manned spacecraft

    GROUNDS, H. / SCHWEISTHAL, R. | AIAA | 1967



    Flight control for manned spacecraft -- Gemini and Apollo -- 1

    Patterson, R. / Hammell, A.K. | Engineering Index Backfile | 1964


    Flight control for manned spacecraft -- Gemini and Apollo -- 2

    Patterson, R. / Hammell, A.K. | Engineering Index Backfile | 1964