Adaptive sliding mode fault-tolerant attitude control for flexible satellites based on T-S fuzzy disturbance modeling

Bin Hang; Beibei Su; Weiwei Deng; Bin Hang; Beibei Su; Weiwei Deng

doi:10.3934/mbe.2023566

Mathematical Biosciences and Engineering

2023, Volume 20, Issue 7: 12700-12717. doi: 10.3934/mbe.2023566

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Research article

Adaptive sliding mode fault-tolerant attitude control for flexible satellites based on T-S fuzzy disturbance modeling

1.
School of Automation, Northwestern Polytechnical University, Xi'an 710072, China
2.
Wuxi Vocational College of Science and Technology, Wuxi 214111, China
3.
Department of Automation, College of Information Engineering, Yangzhou University, Yangzhou 225127, China

Academic Editor: Danilo Pelusi

Received: 23 February 2023 Revised: 19 May 2023 Accepted: 23 May 2023 Published: 30 May 2023

This paper investigates the fault tolerance problem of flexible satellites subject to actuator faults and multiple disturbances. An adaptive sliding mode fault tolerant control (ASMFTC) approach based on Takagi-Sugeno (T-S) fuzzy disturbance observer (TSFDO) is presented for attitude control system (ACS) under loss of actuator effectiveness, environmental disturbance torque and elastic modal generated by flexible appendages. Compared with the traditional disturbance observer based control (DOBC) methods, the T-S fuzzy technology is applied to estimate the unknown nonlinear elastic modal. Then, the energy bounded disturbance is eliminated by designing an adaptive sliding mode controller. The proposed ASMFTC design can guarantee the sliding surface to approach zero. Finally, the effectiveness of the control method proposed in this paper is further verified by comparative simulation.
- satellite,
- disturbance observer,
- fault tolerant control,
- T-S fuzzy model,
- sliding mode control
Citation: Bin Hang, Beibei Su, Weiwei Deng. Adaptive sliding mode fault-tolerant attitude control for flexible satellites based on T-S fuzzy disturbance modeling[J]. Mathematical Biosciences and Engineering, 2023, 20(7): 12700-12717. doi: 10.3934/mbe.2023566

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Abstract

This paper investigates the fault tolerance problem of flexible satellites subject to actuator faults and multiple disturbances. An adaptive sliding mode fault tolerant control (ASMFTC) approach based on Takagi-Sugeno (T-S) fuzzy disturbance observer (TSFDO) is presented for attitude control system (ACS) under loss of actuator effectiveness, environmental disturbance torque and elastic modal generated by flexible appendages. Compared with the traditional disturbance observer based control (DOBC) methods, the T-S fuzzy technology is applied to estimate the unknown nonlinear elastic modal. Then, the energy bounded disturbance is eliminated by designing an adaptive sliding mode controller. The proposed ASMFTC design can guarantee the sliding surface to approach zero. Finally, the effectiveness of the control method proposed in this paper is further verified by comparative simulation.

References

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