This paper puts forward a four-axis dual rotor unmanned aerial vehicle (UAV) and builds the mathematical model. For this model, an aircraft trajectory control method based on robust compensation is presented. To reduce the effects of external disturbances and model parameters' uncertainty, the robust compensator is added to the classical PD control. Simulation results demonstrate that this method can dramatically improve robustness of trajectory control.


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    Title :

    Robust trajectory control of a four-axis dual rotor aircraft


    Contributors:
    Dongxuan, Li (author) / Ting, Zhang (author) / Weijie, Liu (author) / Jinku, Li (author) / Yina, Ren (author) / Di, Mei (author)


    Publication date :

    2014-08-01


    Size :

    481867 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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