29 October 2011 Control and formation flying for the quadrotor UAV
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Proceedings Volume 8205, 2011 International Conference on Photonics, 3D-Imaging, and Visualization; 82052Y (2011) https://doi.org/10.1117/12.906083
Event: 2011 International Conference on Photonics, 3D-imaging, and Visualization, 2011, Guangzhou, China
Abstract
In this paper, control and formation flying for the mini quadrotor UAV are studied. First, the quadrotor UAV is modeled and its simplified mathematical model is given. And then using the traditional PID method in all the designed controller channels, each channel is given in the simulation under different excitation curve. Next the formation problem of the mini quadrotor UAV is analyzed with establishing the dynamic equation of a wingman and the relevant simulation curve is given at last.
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Zhiyong Tang, Zhiyong Tang, Longlong He, Longlong He, Zhongcai Pei, Zhongcai Pei, "Control and formation flying for the quadrotor UAV", Proc. SPIE 8205, 2011 International Conference on Photonics, 3D-Imaging, and Visualization, 82052Y (29 October 2011); doi: 10.1117/12.906083; https://doi.org/10.1117/12.906083
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