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2017 | OriginalPaper | Chapter

Design of Quadrotor Unmanned Aerial Vehicle

Authors : Mofei Wu, Zhigang Cheng, Lin Yang, Lamei Xu

Published in: Intelligent Robotics and Applications

Publisher: Springer International Publishing

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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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Metadata
Title
Design of Quadrotor Unmanned Aerial Vehicle
Authors
Mofei Wu
Zhigang Cheng
Lin Yang
Lamei Xu
Copyright Year
2017
DOI
https://doi.org/10.1007/978-3-319-65298-6_3

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