Abstract The previous Chapter presented a tracking controller of the position and heading of a helicopter based on the linearized helicopter dynamics. The adopted parametric linear model, on which the flight controller is based on, represented the quasi steady state behavior of the helicopter dynamics at hover.


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    Title :

    Nonlinear Tracking Controller Design for Unmanned Helicopters


    Contributors:


    Publication date :

    2011-01-01


    Size :

    33 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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