Linear equivalence of nonlinear systems is applied to a helicopter model. The nonlinear control design obtained allows a transformation of the nonlinear helicopter model to a set of four linear controllable and single-input subsystems to be obtained. The main difference between the application presented and other work is that the authors express the diffeomorphic map of the state-input space in explicit form.


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    Title :

    Helicopter control design using feedback linearization techniques


    Additional title:

    Entwurf einer Hubschrauberregelung bei Verwendung der Rückkopplungslinearisierung


    Contributors:


    Publication date :

    1989


    Size :

    2 Seiten, 7 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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