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Vol. 178, Issue 9, September 2014, pp. 276-281

 

Bullet

 

Non-affine Nonlinear Flight Control System Based on Robust Adaptive Fault-tolerant Control
 

1,2 Zhou Hong-Cheng, 2 Wang Dao-Bo

1 Institute of Information, Jinling Institute of Technology, Nanjing 211169, China
2 College of Automation Engineer, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
1 Tel.: 18913806592, 2 Tel.: 13505184950

E-mail: Zhouhc8@163.com, wdb@nuaa.edu.cn

 

Received: 25 June 2014 /Accepted: 29 August 2014 /Published: 30 September 2014

Digital Sensors and Sensor Sysstems

 

Abstract: For non-affine nonlinear flight control systems, a non-affine nonlinear robust fault tolerance control method is proposed. Here, the fault tolerance control framework is used, and on this basis, observer-based auxiliary system is designed to implicit fault parameters and disturbances information. Then reconfigurable controller is designed using the dynamic of observer-based auxiliary system, which can realize non-affine nonlinear systems robust adaptive fault-tolerant. Simulation results show the effectiveness of the proposed method.

 

Keywords: Non-affine, Nonlinear, Observer, Adaptive, Fault tolerant.

 

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