Unmanned Aerial Vehicle (UAV) flight control is a concerned issue. In order to maintain the flight stability, the UAV fuel allocation method based on centroid balance is proposed in this paper. Firstly, the position calculation approach of the center of mass of UAV is given under different pitch angles. Secondly, according to the actual conditions, a model that minimizes the offset of the center of mass is presented. To solve this problem, an approximate local optimal method is proposed. Finally, the method is applied to the situations of level flight and non-level flight, and the results show that the method is effective.


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    Title :

    UAV Fuel Allocation Method Based on Centroid Balance


    Contributors:
    Yu, Jintao (author) / Xiao, Bing (author) / Xiong, Jiajun (author)


    Publication date :

    2022-04-08


    Size :

    416364 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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