Abstract
The flapping wing micro-air vehicle (FWMAV) is a new type of aerial vehicle which uses mechanical structure to simulate bird flight. The FWMAV possesses the characteristics of small size, light weight, high flight efficiency and no occupation of runway. Firstly, we calculate the aerodynamic lift and drag on the wing surface. Then, through the analysis and summary of the existing FWMAV control technology, the attitude control model of the aerial vehicle is obtained. Besides, the control system based on STM32F103 is designed, which is equipped with a communication module and thus controls the position and flight attitude through the control signals received wirelessly. Finally, the feasibility of the system is verified by MATLAB and Simulink simulation.
L. Jin—This work was supported by the National Natural Science Foundation of China (No. 61703189), by CAS Light of West China Program, by the Team Project of Natural Science Foundation of Qinghai Province, China (No. 2020-ZJ-903), by the National Key Research and Development Program of China (No. 2017YFE0118900), in part by the Sichuan Science and Technology Program (No. 19YYJC1656), in part by the Fundamental Research Funds for the Central Universities (No. lzujbky-2019-89).
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Ma, D., Jin, L., Fu, D., Xiao, X., Liu, M. (2020). On Position and Attitude Control of Flapping Wing Micro-aerial Vehicle. In: Han, M., Qin, S., Zhang, N. (eds) Advances in Neural Networks – ISNN 2020. ISNN 2020. Lecture Notes in Computer Science(), vol 12557. Springer, Cham. https://doi.org/10.1007/978-3-030-64221-1_18
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