Each of following flight phases, namely, launching, flight in space, re-entry, and final descent, must be considered when establishing need of attitude control for each type of vehicle such as ballistic missile, manned satellite, and hypersonic rocket boosted glider; factors to consider in obtaining attitude control and problems of re-entry.


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    Title :

    Attitude control for space vehicles


    Additional title:

    Astronautics


    Contributors:

    Published in:

    Astronautics ; 4 , n 3


    Publication date :

    1959


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Optimal attitude control of space vehicles

    Foy, Jr., W.H. / Lefferts, E.J. | Engineering Index Backfile | 1962


    Attitude Control of Flexible Space Vehicles

    GIACOMO PORCELLI | AIAA | 1972