Aircraft roll command signals are generated as a function of the Microwave Landing System based azimuth, groundtrack, groundspeed and azimuth rate or range distance input parameters. On initial approach, roll command signals are inhibited until a minimum roll command requirement is met. As the aircraft approaches the centerline of the runway, the system reverts to a linear track control.


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    Title :

    Aircraft roll steering command system


    Contributors:

    Publication date :

    1985-08-06


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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