On Aero Control Law Joined Compensatory PID for Glide down to Fixed Low Altitude System and Simulation Researches

De Hai Yu; Dong Cai Qu; Jian Hua Lu; Bin Wen Lu

doi:10.4028/www.scientific.net/AMM.198-199.1021

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 198-199On Aero Control Law Joined Compensatory PID for...

On Aero Control Law Joined Compensatory PID for Glide down to Fixed Low Altitude System and Simulation Researches

Abstract:

In order to improve accuracy of constant altitude fly at low altitude and fly track of glide down to fixed altitude, aeroplane’s control scheme of glide down to fixed low altitude with PID compensatory link were designed. At the same time, the corresponding control laws had been designed. After simple analysis about working principle of the aeroplane’s control system, simulation researches were done to optimize designed control laws, so that achieving expectant requirement. Simulation results show that designed control scheme and control law were accurate and effective.

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Periodical:

Applied Mechanics and Materials (Volumes 198-199)

Pages:

1021-1024

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.198-199.1021

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Online since:

September 2012

Authors:

De Hai Yu, Dong Cai Qu, Jian Hua Lu, Bin Wen Lu

Keywords:

Control Law, Fly Track Control, Glide down to Fixed Altitude, PID

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References

[1] Shenan Yu, Shen Xueren, Li Yunbao: Automatic Flight Control System (National Defense Industry University Press, Beijing 2003), in Chinese.

Google Scholar

[2] Zhang Minglian: Flight Control System (National Defence Industry Press, Beijing 1984), in Chinese.

Google Scholar

[3] Mclean D: Automatic Flight Control Systems (Prentice Hall, New York 1990).

Google Scholar

[4] Wenchuan Yuan. Modern Flight Control. (Beijing Aeronautics and Astronautics Press, Beijing 2004) , in Chinese.

Google Scholar

[5] Christopher Fielding. Advanced Techniques for Clearance of Flight Control Laws. Sprinter, 2002: 180-205.

Google Scholar

[6] Richard C. Dorf & Robert H. Bishop, Translation. Xie Weihong, Zoufeng Xing, Zhang Ming: Modern Control Systems. (Higher Education Press , Beijing 2001) , in Chinese.

Google Scholar

[7] Hou fuhan. Aviation flight control system performance analysis. Modern electronic technology, 10 (9) , 2003: 15-17.

Google Scholar

[8] Wu Shentong, Fei Yuhua: Flight Control System (Beijing Aeronautics and Astronautics Press, Beijing 2005) , in Chinese.

Google Scholar

[9] Christopher Fielding. Advanced Techniques for Clearance of Flight Control Laws. Springer, 2002: 180-205.

Google Scholar

[10] Xie Shihong: MATLAB R2008 Control System Dynamic Simulation Tutorial (Chemical Industry Press , Beijing 2009) , in Chinese.

Google Scholar