This paper presents a framework for attitude command tracking flight controller for a general aviation aircraft using Classical and Incremental Nonlinear Dynamic Inversion approaches. The theoretical background and a framework for attitude tracking flight control framework based on the controllers are presented in this paper. A comparative study of attitude tracking performance of the model dependent Nonlinear Dynamic Inversion Controller and the measurement dependent Incremental Nonlinear Dynamic Inversion Controller for a light aircraft is performed through numerical simulations. Also, Performance evaluation of the Classical and Incremental Nonlinear Dynamic Inversion controllers are carried out under nominal conditions, external disturbances and model uncertainties.


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    Title :

    Attitude Tracking Control of a Light Aircraft Using Classical and Incremental Nonlinear Dynamic Inversion Approaches


    Contributors:


    Publication date :

    2021-06-15


    Size :

    1036856 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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