Fault-tolerant Sliding Mode Controller and Active Vibration Control Design for Attitude Stabilization of a Flexible Spacecraft in the Presence of Bounded Disturbances

Document Type : Original Research Article

Authors

Aerospace Research Institute, Ministry of science, research and technology, Tehran, Iran

Abstract

This paper concerns vibration control and attitude stabilization of a flexible spacecraft with faulty actuators. The PID-based sliding mode fault-tolerant scheme is developed to preserve the system against bounded external disturbances, rigid-flexible body interactions, and partial actuator failures. The proposed control law, which combines the advantages of the PID and SMC, is proposed to enhance the robustness and reduce the steady state errors while reducing complexity and the computational burden and preserving the great properties of the SMC controller. It has been shown that the SMC controller is effective in accommodating different actuator fault scenarios and behaves healthily. Additionally, an active vibration control (AVC) law utilizing a strain rate feedback (SRF) algorithm and piezoelectric (PZT) sensors/actuators is activated during the maneuver to compensate for residual vibrations resulting from attitude dynamics and actuator failures. Numerical simulations demonstrate the proposed schemes' superiority in fault tolerance and robustness compared to conventional approaches.

Keywords

Main Subjects


[1]     D. Lee, "Fault-tolerant finite-time controller for attitude tracking of rigid spacecraft using intermediate quaternion," IEEE Transactions on Aerospace and Electronic Systems, vol. 57, no. 1, pp. 540-553, 2020.
[2]     M. N. Hasan, M. Haris, and S. Qin, "Vibration suppression and fault-tolerant attitude control for flexible spacecraft with actuator faults and malalignments," Aerospace Science and Technology, vol. 120, p. 107290, 2022.
[3]     Q. Hu, X. Zhang, and G. Niu, "Observer-based fault tolerant control and experimental verification for rigid spacecraft," Aerospace Science and Technology, vol. 92, pp. 373-386, 2019.
[4]     G. J. Ducard, Fault-tolerant flight control and guidance systems: Practical methods for small unmanned aerial vehicles. Springer Science & Business Media, 2009.
[5]     A. A. Amin and K. M. Hasan, "A review of fault tolerant control systems: advancements and applications," Measurement, vol. 143, pp. 58-68, 2019.
[6]     Q. Hu, X. Shao, and L. Guo, "Adaptive fault-tolerant attitude tracking control of spacecraft with prescribed performance," IEEE/ASME Transactions on Mechatronics, vol. 23, no. 1, pp. 331-341, 2017.
[7]     D. Hyland, J. Junkins, and R. Longman, "Active control technology for large space structures," Journal of Guidance, Control, and Dynamics, vol. 16, no. 5, pp. 801-821, 1993.
[8]     S. Firuzi and S. Gong, "Attitude control of a flexible solar sail in low Earth orbit," Journal of Guidance, Control, and Dynamics, vol. 41, no. 8, pp. 1715-1730, 2018.
[9]     M. Shahravi, M. Kabganian, and A. Alasty, "Adaptive robust attitude control of a flexible spacecraft," International Journal of Robust and Nonlinear Control: IFAC‐Affiliated Journal, vol. 16, no. 6, pp. 287-302, 2006.
[10]   Y. Zhu, L. Guo, J. Qiao, and W. Li, "An enhanced anti-disturbance attitude control law for flexible spacecrafts subject to multiple disturbances," Control Engineering Practice, vol. 84, pp. 274-283, 2019.
[11]   R. Chai, A. Tsourdos, H. Gao, Y. Xia, and S. Chai, "Dual-loop tube-based robust model predictive attitude tracking control for spacecraft with system constraints and additive disturbances," IEEE Transactions on Industrial Electronics, vol. 69, no. 4, pp. 4022-4033, 2021.
[12]   C. Zhang, M.-Z. Dai, J. Wu, B. Xiao, B. Li, and M. Wang, "Neural-networks and event-based fault-tolerant control for spacecraft attitude stabilization," Aerospace Science and Technology, vol. 114, p. 106746, 2021.
[13]   A.-M. Zou and K. D. Kumar, "Adaptive fuzzy fault-tolerant attitude control of spacecraft," Control Engineering Practice, vol. 19, no. 1, pp. 10-21, 2011.
[14]   Q. Hu, B. Xiao, and Y. Zhang, "Fault-tolerant attitude control for spacecraft under loss of actuator effectiveness," Journal of Guidance, Control, and Dynamics, vol. 34, no. 3, pp. 927-932, 2011.
[15]   D. Wenjie, W. Dayi, and L. Chengrui, "Integral sliding mode fault‐tolerant control for spacecraft with uncertainties and saturation," Asian Journal of Control, vol. 19, no. 1, pp. 372-381, 2017.
[16]   Q. Hu, "Robust adaptive sliding-mode fault-tolerant control with L2-gain performance for flexible spacecraft using redundant reaction wheels," IET control theory & applications, vol. 4, no. 6, pp. 1055-1070, 2010.
[17]   Q. Hu and B. Xiao, "Fault-tolerant sliding mode attitude control for flexible spacecraft under loss of actuator effectiveness," Nonlinear Dynamics, vol. 64, no. 1, pp. 13-23, 2011.
[18]   S. Varma and K. Kumar, "Fault tolerant satellite attitude control using solar radiation pressure based on nonlinear adaptive sliding mode," Acta Astronautica, vol. 66, no. 3-4, pp. 486-500, 2010.
[19]   M. Labbadi, Y. Boukal, and M. Cherkaoui, "High Order Fractional Controller Based on PID-SMC for the QUAV Under Uncertainties and Disturbance," in Advanced Robust Nonlinear Control Approaches for Quadrotor Unmanned Aerial Vehicle: Springer, 2022, pp. 165-190.
[20]   Q. Hu and G. Ma, "Vibration suppression of flexible spacecraft during attitude maneuvers," Journal of guidance, control, and dynamics, vol. 28, no. 2, pp. 377-380, 2005.
[21]   G. Song and B. N. Agrawal, "Vibration suppression of flexible spacecraft during attitude control," Acta Astronautica, vol. 49, no. 2, pp. 73-83, 2001.
[22]   M. Shahravi and M. Azimi, "A Hybrid Scheme of Synthesized Sliding Mode/Strain Rate Feedback Control Design for Flexible Spacecraft Attitude Maneuver Using Time Scale Decomposition," International Journal of Structural Stability and Dynamics, vol. 16, no. 02, p. 1450101, 2016.
[23]   J.-J. Xiong and G. Zhang, "Discrete-time sliding mode control for a quadrotor UAV," Optik, vol. 127, no. 8, pp. 3718-3722, 2016.
[24]   X. Wang, S. Sun, E.-J. van Kampen, and Q. Chu, "Quadrotor fault tolerant incremental sliding mode control driven by sliding mode disturbance observers," Aerospace Science and Technology, vol. 87, pp. 417-430, 2019.
[25]   T. Lv, J. Zhou, Y. Wang, W. Gong, and M. Zhang, "Sliding mode based fault tolerant control for autonomous underwater vehicle," Ocean Engineering, vol. 216, p. 107855, 2020.
[26]   Q. Liu, M. Liu, and J. Yu, "Adaptive fault-tolerant control for attitude tracking of flexible spacecraft with limited data transmission," IEEE Transactions on Systems, Man, and Cybernetics: Systems, vol. 51, no. 7, pp. 4400-4408, 2019.
[27]   B. Guo and Y. Chen, "Adaptive fast sliding mode fault tolerant control integrated with disturbance observer for spacecraft attitude stabilization system," ISA transactions, vol. 94, pp. 1-9, 2019.
[28]   Q. Hu, "Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits," Nonlinear Dynamics, vol. 55, no. 4, pp. 301-321, 2009.
[29]   A. T. Azar and Q. Zhu, Advances and applications in sliding mode control systems. Springer, 2015.
[30]   A. Noordin, M. A. Mohd Basri, Z. Mohamed, and I. Mat Lazim, "Adaptive PID controller using sliding mode control approaches for quadrotor UAV attitude and position stabilization," Arabian Journal for Science and Engineering, vol. 46, no. 2, pp. 963-981, 2021.
[31]   M. T. Hamayun, C. Edwards, and H. Alwi, Fault tolerant control schemes using integral sliding modes. Springer, 2016.
[32]   M. Shahravi and M. Azimi, "Attitude and vibration control of flexible spacecraft using singular perturbation approach," International Scholarly Research Notices, vol. 2014, 2014.
Volume 5, Issue 1
June 2022
Pages 85-91
  • Receive Date: 22 September 2022
  • Revise Date: 01 November 2022
  • Accept Date: 05 November 2022
  • First Publish Date: 05 November 2022