Tilt-rotor UAVs are exceptionally suitable for near-ground unmanned transportation and other fields because of their helicopter mode, transition mode and fixed-wing mode. However, the tilt-rotor transition on trajectory planning presents a challenge, as performance constraints of different modes must be considered and a trajectory planning algorithm is required to optimize a collision-free and short trajectory with low fuel consumption and small cost. To address these challenges, this paper adds performance constraints of the tilt-rotor UAV to the hybrid algorithm by combining the A* algorithm and the artificial potential field method; meanwhile, the rationality of trajectory planning is improved by setting the tilt-rotor transition region separately in the global. Simulation results show that a reasonable trajectory can be planned by setting the tilt-transition region by itself and using a hybrid algorithm.


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    Title :

    Trajectory Planning of Tilt-Rotor UAV Based on Hybrid Algorithm


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Lee, Sangchul (editor) / Han, Cheolheui (editor) / Choi, Jeong-Yeol (editor) / Kim, Seungkeun (editor) / Kim, Jeong Ho (editor) / Ren, Binwu (author) / Wang, Bo (author) / Zhang, Xiayang (author) / Zhao, Qijun (author)

    Conference:

    Asia-Pacific International Symposium on Aerospace Technology ; 2021 ; Korea (Republic of) November 15, 2021 - November 17, 2021



    Publication date :

    2022-09-30


    Size :

    13 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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