The report describes an experimental flight guidance system for controlling an aircraft's lateral axis during Instrumental Landing System approaches and landings. The system incorporates an inertial damping term in the form of drift angle, accomplishes runway alignment through the forward slip maneuver, provides roll out guidance through the rudder, and wings level control through the ailerons. (Author)


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    Title :

    Experimental Lateral Landing Computer with Inertial Stabilization


    Contributors:

    Publication date :

    1971


    Size :

    84 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    Emergency landing using inertial sensors

    CUTLER MARK JOHNSON | European Patent Office | 2019

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    Emergency landing using inertial sensors

    CUTLER MARK JOHNSON | European Patent Office | 2017

    Free access