Mathematical model of space vehicle is formulated; for wide choice of performance criteria, optimal attitude control is shown by Pontryagin's Maximum Principle to be so-called bang-bang operation.


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    Title :

    Optimal attitude control of space vehicles


    Additional title:

    IRE East Coast Conference -- Tech Paper


    Contributors:

    Conference:

    IRE East Coast Conference on Aerospace and Navigational Electronics -- Meeting ; 1962 Control



    Publication date :

    1962


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Attitude control for space vehicles

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    Reaction Wheel Attitude Control for Space Vehicles

    R. W. Froelich / H. Patapoff | NTIS | 1959