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Active Fault Tolerant Control Scheme for Satellite Attitude Systems: Multiple Actuator Faults Case

  • Zhifeng Gao
  • Zepeng Zhou
  • Guoping Jiang
  • Moshu Qian
  • Jinxing Lin
Regular Papers Control Theory and Applications
  • 28 Downloads

Abstract

In this paper, an active fault tolerant control (FTC) design approach is proposed for the satellite attitude systems with exogenous disturbance and multiple actuator faults. Firstly, the nonlinear attitude system model of rigid satellite with multiple actuator faults is given. Next, an actuator fault diagnosis scheme, including a fault detection module and a fault estimation module, is given so as to detect the time of unknown actuator faults occurred and obtain their estimation values. Then, a terminal sliding mode-based fault tolerant attitude controller is designed using backstepping control technique, which guarantees that the closed-loop attitude systems of rigid satellite are asymptotically stable in the presence of multiple actuator faults. Numerical simulations illustrate the good performance of active FTC proposed in this study.

Keywords

Fault detection fault estimation fault tolerant control satellite attitude systems 

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References

  1. [1]
    W. MacKunis, F. Leve, P. M. Patre, N. Fitz-Coyd, and W. E. Dixon, “Adaptive neural network-based satellite attitude control in the presence of CMG uncertainty,” Aerospace Science and Technology, vol. 54, no. 7, pp. 218–228, July 2016.CrossRefGoogle Scholar
  2. [2]
    M. S. Qian, B. Jiang, and H. H. T. Liu, “Dynamic surface active fault tolerant control design for the attitude control systems of UAV with actuator fault,” International Journal of Control, Automation, and Systems, vol. 14, no. 3, pp. 723–732, June 2016.CrossRefGoogle Scholar
  3. [3]
    Y. H. Cheng, B. Jiang, N. Y. Lu, T. Wang, and Y. Xing, “Incremental locally linear embedding-based fault detection for satellite attitude control systems,” Journal of the Franklin Institute, vol. 353, no. 1, pp. 17–36, January 2016.MathSciNetCrossRefGoogle Scholar
  4. [4]
    D. Hu, A. Sarosh, and Y. F. Dong, “A novel KFCM based fault diagnosis method for unknown faults in satellite reaction wheels,” ISA Transactions, vol. 51, no. 2, pp. 309–316, February 2012.CrossRefGoogle Scholar
  5. [5]
    C. Y. Gao, Q. Zhao, and G. R. Duan, “Robust actuator fault diagnosis scheme for satellite attitude control systems,” Journal of the Franklin Institute, vol. 350, no. 9, pp. 2560–2580, September 2013.MathSciNetCrossRefzbMATHGoogle Scholar
  6. [6]
    Y. J. Ma, B. Jiang, G. Tao, and Y. H. Cheng, “Actuator failure compensation and attitude control for rigid satellite by adaptive control using quaternion feedback,” Journal of the Franklin Institute, vol. 351, no. 1, pp. 296–314, January 2014.MathSciNetCrossRefzbMATHGoogle Scholar
  7. [7]
    D. Zhao, H. Yang, B. Jiang, and L. Y. Wen, “Attitude stabilization of a flexible spacecraft under actuator complete failure,” Acta Astronautica, vol. 123, no. 6, pp. 129–136, June-July 2016.CrossRefGoogle Scholar
  8. [8]
    Q. L. Hu and X. D. Shao, “Smooth finite-time fault-tolerant attitude tracking control for rigid spacecraft,” Aerospace Science and Technology, vol. 55, no. 8, pp. 144–157, August 2016.CrossRefGoogle Scholar
  9. [9]
    J. L. Lan and R. J. Patton, “A new strategy for integration of fault estimation within fault-tolerant control,” Automatica, vol. 69, no. 11, pp. 48–59, November 2016.MathSciNetCrossRefzbMATHGoogle Scholar
  10. [10]
    C. Y. Gao and G. R. Duan, “Fault diagnosis and fault tolerant control for nonlinear satellite attitude control systems,” Aerospace Science and Technology, vol. 33, no. 1, pp. 9–15, February 2014.CrossRefGoogle Scholar
  11. [11]
    J. Jiang and X. Yu, “Fault-tolerant control systems: a comparative study between active and passive approaches,” Annual Reviews in Control, vol. 36, no. 1, pp. 60–72, January 2012.CrossRefGoogle Scholar
  12. [12]
    J. K. Lee, Y. H. Choi, and J. B. Park, “Sliding mode tracking control of mobile robots with approach angle in cartesian coordinates,” International Journal of Control, Automation, and Systems, vol. 13, no. 3, pp. 718–724, March 2015.CrossRefGoogle Scholar
  13. [13]
    Z. K. Song, H. X. Li, and K. B. Sun, “Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique,” ISA Transactions, vol. 53, no. 1, pp. 117–124, January 2014.CrossRefGoogle Scholar
  14. [14]
    M. Chen and J. Yu, “Adaptive dynamic surface control of NSVs with input saturation using a disturbance observer,” Chinese Journal of Aeronautics, vol. 28, no. 3, pp. 853–864, March 2015.CrossRefGoogle Scholar
  15. [15]
    X. Q. Chen, Y. H. Ma, F. Wang, and Y. H. Geng, “Research on improved integrated FDD/FTC with effectiveness factors,” Journal of Systems Engineering and Electronics, vol. 23, no. 5, pp. 768–774, May 2012.CrossRefGoogle Scholar
  16. [16]
    G. Chen and Y. D. Song, “Robust fault-tolerant cooperative control of multi-agent systems: a constructive design method,” Journal of the Franklin Institute, vol. 352, no. 10, pp. 4045–4066, October 2015.MathSciNetCrossRefGoogle Scholar
  17. [17]
    Q. L. Hu, B. Li, and J. T. Qi, “Disturbance observer based finite-time attitude control for rigid spacecraft under input saturation,” Aerospace Science and Technology, vol. 39, no. 12, pp. 13–21, December 2014.CrossRefGoogle Scholar

Copyright information

© Institute of Control, Robotics and Systems and The Korean Institute of Electrical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature 2018

Authors and Affiliations

  • Zhifeng Gao
    • 1
    • 2
  • Zepeng Zhou
    • 1
    • 2
  • Guoping Jiang
    • 1
    • 2
  • Moshu Qian
    • 3
    • 4
  • Jinxing Lin
    • 1
    • 2
  1. 1.College of AutomationNanjing University of Posts and TelecommunicationsNanjingChina
  2. 2.Jiangsu Engineering Laboratory for Intelligent IOT RobotsNanjingChina
  3. 3.College of Electrical Engineering and Control ScienceNanjing Tech UniversityNanjingChina
  4. 4.State Key Laboratory of Mechanics and Control of Mechanical StructuresNanjing University of Aeronautics and AstronauticsNanjingChina

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