The objective of this chapter is to develop a unified actuator nonlinearity compensation scheme for an aircraft augmented with SJs operating at a wide range of conditions, including both low and high AoA. The motivation for such a design is the intrinsically complicated nonlinear characteristic of a SJ when used for an aircraft operating in a wide range of AoA.


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    Title :

    Adaptive Synthetic Jet Actuation for Aircraft Control


    Additional title:

    Studies in Systems, Decision and Control


    Contributors:


    Publication date :

    2021-07-23


    Size :

    17 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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