The minor loop and minor loop support modules which maintain correct vehicle attitude control by generating vehicle attitude error signals were verified. The logic is checked during boost and orbit (unusual timing situations necessitate the additional orbit checks) and the constants used by these modules checked at every point during the flight. Since the same logic instructions are used throughout the flight with only the constants changing, verification of the logic at two points and the constants at all points verify the logic throughout the flight.


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    Title :

    Launch vehicle attitude control



    Publication date :

    1975-04-15


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :





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