Automatic control of aircraft during landing is discussed and a new structure of automatic landing system (ALS) is designed using the dynamic inversion concept and proportional-integral-derivative (PID) controllers in conventional and fuzzy variants. Theoretical results are validated by numerical simulations in the absence or presence of wind shears and sensor errors.


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    Title :

    Automatic Control of Aircraft in Longitudinal Plane During Landing


    Contributors:
    Lungu, R. (author) / Lungu, M. (author) / Grigorie, L. T. (author)


    Publication date :

    2013-04-01


    Size :

    15550699 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



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