In this paper, a pre-defined performance tracking control method based on the safe flight boundary of a Hybrid Vertical Take-Off and Landing (VTOL) UAV is presented. Firstly, longitudinal flight model of hybrid VTOL UAV is modeled, and secondly, based on the UAV power constraint, the UAV's angle of attack-velocity safety boundary is established. Then, the performance function is designed based on the safety boundary. The VTOL UAV boundary protection is implemented using a pre-defined performance control method. Finally, the theoretical analysis and simulation experiments verify the effectiveness of the method in this paper.


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    Title :

    Boundary Protection Control of a Hybrid Vertical Take-Off and Landing UAV


    Contributors:
    Chen, Tongqing (author) / Wu, Dawei (author) / Xv, Shenjie (author) / Wang, Bolin (author) / Huang, Xiaoqi (author)


    Publication date :

    2023-05-08


    Size :

    796236 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English