Abstract
This paper designs the dynamic system and main control circuit of quadrotor unmanned aerial vehicle (UAV). Power system of the quadrotor UAV includes brushless DC motor (BDCM), matching paddle, power lithium battery and drive circuit of (BDCM). Its main control hardware circuit includes the main controller minimum system, the sensor module, the wireless communication module and the power module. The attitude algorithm and attitude control algorithm are designed. The Kalman filter algorithm is used to calculate the attitude of quadrotor UAV. The cascade PID control algorithm is used to control attitude. Finally, a quadrotor UAV prototype was trial-produced, and the tested results show that the aerial vehicle meets the design requirements.
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Wu, M., Cheng, Z., Yang, L., Xu, L. (2017). Design of Quadrotor Unmanned Aerial Vehicle. In: Huang, Y., Wu, H., Liu, H., Yin, Z. (eds) Intelligent Robotics and Applications. ICIRA 2017. Lecture Notes in Computer Science(), vol 10464. Springer, Cham. https://doi.org/10.1007/978-3-319-65298-6_3
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DOI: https://doi.org/10.1007/978-3-319-65298-6_3
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Publisher Name: Springer, Cham
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Online ISBN: 978-3-319-65298-6
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