The results of a computer study on four roll-out guidance control laws and a nosewheel steering configuration is included herein. Beam convergence, ground speed, and crosswind effects were included in the simulation. (Author)


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    Title :

    Landing and Takeoff Roll-Out Augmentation


    Contributors:
    V. Muehter (author)

    Publication date :

    1974


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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