Flight Control System for UAV Based on Simulink

Guo Dong Jin; Li Bin Lu; Juan Liang; Xiao Fei Zhu

doi:10.4028/www.scientific.net/AMR.709.662

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 709Flight Control System for UAV Based on Simulink

Flight Control System for UAV Based on Simulink

Abstract:

Most UAV flight control system simulation was used for evaluating the quality of UAV and designing it, however, the results failed to conform to actual flight laws. According to the need of UAV simulator in actually, a new way which was convenient for engineering computing and appropriated for simulation training was built for simulating flight control system. With the actual flight figures, flight parameters were modified by Least squares method curve fitting. The system offers a way for developing UAV simulation training system, thus of great value in both theory and practice.

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Periodical:

Advanced Materials Research (Volume 709)

Pages:

662-666

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.709.662

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Online since:

June 2013

Authors:

Guo Dong Jin, Li Bin Lu, Juan Liang, Xiao Fei Zhu

Keywords:

Flight Control System, Simulation, Six-Degree-of-Freedom Equations, Unmanned Aerial Vehicle (UAV)

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References

[1] Chen Bing, Zhu Jihong, and Sun Zengqi,"PC Based Unmanned Aerial Vehicle Simulation System" Journal of system simulation Vol. 14, No.5, pp.614-615, May. 2002. (in Chinese)

Google Scholar

[2] Wen Chuanyuan Author, "Model flight control" BeiJing：Beijing University of Aeronautics and Astronautics Press, p.15~33, Oct. (2004)

Google Scholar

[3] Yang Chao. "High Order Linearized Model of Helicopter Flight Dynamics" Flight Dynamics，Vol. 18, No.1 pp.1-4, Mar. 2000 (in Chinese)

Google Scholar

[4] Yang Xin, Wang Xiaohu, Shen Gongzhang. "Modeling and Simulation Research of Six-Degree-of Freedom Fighter". Journal of system simulation Vol. 12, No.3, pp.210-213, May. 2000. (in Chinese)

Google Scholar

[5] Ni Xiaoping, Zhu Guoming, Mei Bin. "Investigation of Verifying Method on the Helicopter Flight Dynamics Models" Flight Dynamics，Vol. 20, No.3, pp.21-24, Sep. 2002 (in Chinese)

Google Scholar