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Vol. 178, Issue 9, September 2014, pp. 264-269

 

Bullet

 

The Aircraft Attitude Robust Inversion Fault-tolerant Control Based on Observer
 

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

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

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

 

Received: 23 June 2014 /Accepted: 29 August 2014 /Published: 30 September 2014

Digital Sensors and Sensor Sysstems

 

Abstract: For attitude control system, based on instruction filter back-stepping techniques, a robust fault-tolerant control method is proposed. Firstly, attitude control system mathematical model is given, on this basis, the attitude control system under the modeling errors caused by uncertainty, external disturbances and control surfaces faults are considered. The fault tolerant control design involves two main units, one is auxiliary system design, the other is controller design using the auxiliary system. Finally, the simulation results show that the proposed method can make the tracking performance for flight control system.

 

Keywords: Attitude, Instruction filter, Back-stepping, Fault tolerant, Tracking.

 

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