Fault-Tolerant Control System Design of UAV Based on Dissimilar Redundancy

Zhen Duan; Dong Hai Qiu; Jiu Zhou Gao

doi:10.4028/www.scientific.net/AMM.397-400.1434

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 397-400Fault-Tolerant Control System Design of UAV Based...

Fault-Tolerant Control System Design of UAV Based on Dissimilar Redundancy

Abstract:

Based on the idea of dissimilar redundant design, a control structure with the fault-tolerant control function even the UAV lateral control loop that is under the state of the aileron fault is researched. The results show that the classical control can not maintain the required yaw, while the dissimilar redundant control can maintain it. The methods is simple, but can effectively avoid the flight accidents caused by aileron fault, so that to improve the safety and reliability of the flight.

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Periodical:

Applied Mechanics and Materials (Volumes 397-400)

Pages:

1434-1437

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.397-400.1434

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Online since:

September 2013

Authors:

Zhen Duan, Dong Hai Qiu, Jiu Zhou Gao

Keywords:

Dissimilar Redundancy, Fault-Tolerant Control, UAV, Yaw Keeping/Control

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References

[1] JIA Cai-juan, ZHU Xiao-ping, ZHOU Zhou. Study on Sensor and Actuator Fault Diagnosis. JOURNAL OF SYSTEM SIMULATION, 17(6): 1435-1437. (2005)(in Chinese).

Google Scholar

[2] JIN C J, XIAO Y L. Flight Control. Beijing: National Defence Industry Press. (1999) (in Chinese).

Google Scholar

[3] WEN C Y. Modern Flight Control System. Beijing: Beijing University of Aeronautics and Astronautics Press , 2005. (1992) (in Chinese).

Google Scholar

[4] SHEN G Z, ZHANG R. DSS of the DFCS's Redundant Scheme Design . Journal of Beijing University of Aeronautics and Astronautics, 25 (3) : 363-366. (1999) (in Chinese).

Google Scholar

[5] WU S T, FEI Y H. Flight Control System. Beijing: Beijing University of Aeronautics and Astronautics Press , 2005. (in Chinese).

Google Scholar