25 October 2017 Design and simulation of flight control system for man-portable micro reconnaissance quadcopter
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Proceedings Volume 10460, AOPC 2017: Optoelectronics and Micro/Nano-Optics; 104600K (2017) https://doi.org/10.1117/12.2283377
Event: Applied Optics and Photonics China (AOPC2017), 2017, Beijing, China
Abstract
The quadcopter has been widely used in the field of aerial photography and environmental detection, because of its advantages of VTOL, simple structure, and easy-control. In the field of urban anti-terrorism or special operations, micro reconnaissance quadcpter has its unique advantages such as all-weather taking off and landing, small noise and so on, and it is very popular with special forces and riot police. This paper aims at the flight control problem of the micro quadcopter, for the purposes of attitude stabilization control and trajectory tracking control of the micro quadcopter, first, the modeling of the micro quadcopter is presented. And using the MATLAB/SIMULINK toolbox to build the flight controller of the micro quadcopter, and then simulation analysis and real flight test are given. The results of the experiment show that the designed PID controller can correct the flight attitude shift effectively and track the planned tracks well, and can achieve the goal of stable and reliable flight of the quadcopter. It can be a useful reference for the flight control system design of future special operations micro UAV.
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Xinfan Yin, Xinfan Yin, Daibing Zhang, Daibing Zhang, Qiang Fang, Qiang Fang, Lincheng Shen, Lincheng Shen, } "Design and simulation of flight control system for man-portable micro reconnaissance quadcopter", Proc. SPIE 10460, AOPC 2017: Optoelectronics and Micro/Nano-Optics, 104600K (25 October 2017); doi: 10.1117/12.2283377; https://doi.org/10.1117/12.2283377
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