Robust H∞ fault tolerant control for quadrotor attitude regulation

Author:

Li Cong1,Jing Hui23,Bao Jiading2,Sun Shanlin1,Wang Rongrong4

Affiliation:

1. Guilin University of Aerospace Technology, Guilin, P.R. China

2. Guilin University of Electronic Technology, Guilin, P.R. China

3. Southeast University, Nanjing, P.R. China

4. Shanghai Jiao Tong University, Shanghai, P.R. China

Abstract

This article investigates the robust H fault tolerant control of quadrotor attitude regulation. The hover stability is heavily dependent on the thrust forces generated by the four rotors of the quadrotor. If faults occur in the rotors, the quadrotor becomes unstable, and possibly out of control. To this end, this article proposes a robust H fault tolerant control schema, consisting of two level controllers, for regulation of the quadrotor attitude. The functions of the upper level controller and lower level controller are to generate the desired control input, and obtain the real input of the four rotors, respectively. In addition, the external disturbances are considered and attenuated by the controller. The simulation details are presented, and the effectiveness of the proposed control schema is verified.

Funder

Opening Project of Guangxi Colleges and Universities Key Laboratory of UAV Remote Sensing

Natural Science Foundation of Guangxi Province

National Natural Science Foundation of China

Guangxi key laboratory of Manufacturing System and Advanced Manufacturing Technology

Publisher

SAGE Publications

Subject

Mechanical Engineering,Control and Systems Engineering

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