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Proceedings Paper

Research on flight stability performance of rotor aircraft based on visual servo control method
Author(s): Yanan Yu; Jing Chen
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Paper Abstract

control method based on visual servo feedback is proposed, which is used to improve the attitude of a quad-rotor aircraft and to enhance its flight stability. Ground target images are obtained by a visual platform fixed on aircraft. Scale invariant feature transform (SIFT) algorism is used to extract image feature information. According to the image characteristic analysis, fast motion estimation is completed and used as an input signal of PID flight control system to realize real-time status adjustment in flight process. Imaging tests and simulation results show that the method proposed acts good performance in terms of flight stability compensation and attitude adjustment. The response speed and control precision meets the requirements of actual use, which is able to reduce or even eliminate the influence of environmental disturbance. So the method proposed has certain research value to solve the problem of aircraft’s anti-disturbance.

Paper Details

Date Published: 7 November 2016
PDF: 7 pages
Proc. SPIE 10141, Selected Papers of the Chinese Society for Optical Engineering Conferences held July 2016, 101411V (7 November 2016); doi: 10.1117/12.2256478
Show Author Affiliations
Yanan Yu, Tianjin Univ. of Technology and Education (China)
Jing Chen, Tianjin Univ. of Technology and Education (China)

Published in SPIE Proceedings Vol. 10141:
Selected Papers of the Chinese Society for Optical Engineering Conferences held July 2016
Yueguang Lv; Weimin Bao; Guangjun Zhang, Editor(s)

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