Control scheme to minimize lateral drift and concurrently to maintain structural load limits of vehicle is presented and compared with conventional vehicle attitude control schemes; guidance problem is solved by directing acceleration vector in manner that will cause vehicle to move from its present state to desired future state; conventional vehicle attitude control schemes insure stable rotational dynamic behavior of vehicle by attempting to bring its attitude into coincidence with desired attitude; it also is independent of vehicle attitude feedback.


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    Title :

    Acceleration vector attitude control system


    Additional title:

    J Spacecraft Rockets


    Contributors:

    Published in:

    Publication date :

    1968


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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