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Adaptive Sliding Mode Fault Tolerant Control of Spacecraft with Actuator Effectiveness

  • Anliang LiEmail author
  • Henghai Fan
  • Shaoyu Zhang
  • Heng Wang
  • Jun Wei
  • Xiaobo Hui
  • Sicong Guo
  • Qi Liu
Conference paper
  • 12 Downloads
Part of the Advances in Intelligent Systems and Computing book series (AISC, volume 1146)

Abstract

Under the extensive application of the spacecraft, an adaptive sliding mode fault tolerant controller is proposed for a spacecraft with the actuator effectiveness and external disturbance. In this approach, the attitude fault-tolerant control scheme based on the sliding mode control theory is design to achieve fault-tolerant control and external disturbance rejection. Then, considering the unknown parameters problem of the actuator and disturbance, adaptive methods is introduced to real-time estimate the unknown parameters, which improve the robustness and practicality of the controller. Finally, the stability of the proposed controller is proved based on the Lyapunov theory and the simulation results show the method with strong fault tolerance for spacecraft actuator failure.

Keywords

Actuator effectiveness Control constraint Fault tolerant control Adaptive sliding mode control 

References

  1. 1.
    Zou, A.M., Kumar, K.D.: Robust attitude coordination control for spacecraft formation flying under actuator failures. J. Guid. Control Dyn. 35(4), 1247–1255 (2012)CrossRefGoogle Scholar
  2. 2.
    Boskovic, J.D., Bergstrom, S.E., Mehra, R.K.: Robust integrated flight control design under failures, damage, and state–dependent disturbances. J. Guid. Control Dyn. 28(5), 902–917 (2005)CrossRefGoogle Scholar
  3. 3.
    Godard, Kumar, K.D.: Fault tolerant reconfigurable satellite formations using adaptive variable structure techniques. J. Guid. Control Dyn. 33(3), 969–984 (2010)Google Scholar
  4. 4.
    Varma, S., Kumar, K.D.: Fault tolerant satellite attitude control using solar radiation pressure based on nonlinear adaptive sliding mode. Acta Astronaut. 66(3–4), 486–500 (2009)Google Scholar
  5. 5.
    Lee, H., Kim, Y., Kim, H.S.: Satellite attitude control with a modified iterative learning law for the decrease in the effectiveness of the actuator. Int. J. Aeronaut. Space Sci. 11(2), 87–97 (2010)CrossRefGoogle Scholar
  6. 6.
    Noumi, A., Takahashi, M.: Fault tolerant attitude control systems for satellite equipped with control moment gyros. In: AIAA Guidance, Navigation, and Control Conference. AIAA 2013, p. 5119. AIAA, Boston (2013)Google Scholar
  7. 7.
    Chandrasekar, S., Suresh, S., Sundararajan, N., et al.: An intelligent fault tolerant satellite attitude control system without hardware redundancies. In: 11th International Conference on Control, Automation, Robotics and Vision, pp. 50–56. IEEE, Singapore (2010)Google Scholar
  8. 8.
    De Ruiter, A.: A fault-tolerant magnetic spin stabilizing controller for the JC2Sat-FFmission. Acta Astronaut. 68, 160–171 (2010)CrossRefGoogle Scholar
  9. 9.
    Li, Z., Yang, X.B., Gao, H.J.: Autonomous impulsive rendezvous for spacecraft under orbital uncertainty and thruster faults. J. Franklin Inst. Eng. Appl. Math. 350, 2455–2473 (2013)MathSciNetCrossRefGoogle Scholar
  10. 10.
    Wei, J.B., Liu, K., Wu, J.J.: Adaptive sliding mode attitude controller for satellites three-axis-stabilized in inertial frame. J. Control Decis. 28(8), 1231–1236 (2013)Google Scholar
  11. 11.
    Hu, Q.L., Zhang, A.H., Li, B.: Adaptive variable structure fault tolerant control of rigid spacecraft under thruster faults. Acta Aeronautica ET Astronautica Sinica 34(4), 909–918 (2013)Google Scholar
  12. 12.
    Cai, W., Liao, X.H., Song, Y.D.: Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft. J. Guid. Control Dyn. 31(5), 1456–1463 (2008)CrossRefGoogle Scholar

Copyright information

© Springer Nature Switzerland AG 2020

Authors and Affiliations

  • Anliang Li
    • 1
    • 2
    Email author
  • Henghai Fan
    • 1
  • Shaoyu Zhang
    • 1
  • Heng Wang
    • 1
  • Jun Wei
    • 1
  • Xiaobo Hui
    • 1
  • Sicong Guo
    • 1
  • Qi Liu
    • 1
  1. 1.State Key Laboratory of Astronautic DynamicsXi’anChina
  2. 2.College of System EngineeringNational University of Defense TechnologyChangshaChina

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