[1] Dong R.-Q., Wu A.-G., Zhang Y. and Duan G.-R., “Anti-unwinding sliding mode attitude control via two modified Rodrigues parameter sets for spacecraft,” Automatica, 2021, vol. 129, p. 109642.
[2] Wenjie D., Dayi W. and Chengrui L., “Integral sliding mode fault‐tolerant control for spacecraft with uncertainties and saturation,” Asian Journal of Control, 2017, vol. 19, no. 1, pp. 372-381.
[3] Zhang X. and Huang W., “Adaptive sliding mode fault tolerant control for interval Type-2 fuzzy singular fractional-order systems,” Journal of Vibration and Control, 2022, vol. 28, no. 3-4, pp. 465-475.
[4] Aydin M. N. and Coban R., “PID sliding surface-based adaptive dynamic second-order fault-tolerant sliding mode control design and experimental application to an electromechanical system,” International Journal of Control, 2022, vol. 95, no. 7, pp. 1767-1776.
[5] Khan A. H. and Li S., “Sliding mode control with PID sliding surface for active vibration damping of pneumatically actuated soft robots,” IEEE Access, 2020, vol. 8, pp. 88793-88800.
[6] Jiang Y., Hu Q. and Ma G., “Adaptive backstepping fault-tolerant control for flexible spacecraft with unknown bounded disturbances and actuator failures,” ISA transactions, 2010, vol. 49, no. 1, pp. 57-69.
[7] Zou T., Wu H., Sun W. and Zhao Z., “Adaptive neural network sliding mode control of a nonlinear two‐degrees‐of‐freedom helicopter system,” Asian Journal of Control, 2022,
[8] Huo B., Xia Y., Yin L. and Fu M., “Fuzzy adaptive fault-tolerant output feedback attitude-tracking control of rigid spacecraft,” IEEE Transactions on Systems, Man, and Cybernetics: Systems, 2016, vol. 47, no. 8, pp. 1898-1908.
[9] Chai R., Tsourdos A., Gao H., Xia Y. and Chai S., “Dual-loop tube-based robust model predictive attitude tracking control for spacecraft with system constraints and additive disturbances,” IEEE Transactions on Industrial Electronics, 2021, vol. 69, no. 4, pp. 4022-4033.
[10] Rubagotti M., Estrada A., Castaños F., Ferrara A. and Fridman L., “Integral sliding mode control for nonlinear systems with matched and unmatched perturbations,” IEEE Transactions on Automatic Control, 2011, vol. 56, no. 11, pp. 2699-2704.
[11] Gao Z., Han B., Jiang G., Lin J. and Xu D., “Active fault tolerant control design approach for the flexible spacecraft with sensor faults,” Journal of the Franklin Institute, 2017, vol. 354, no. 18, pp. 8038-8056.
[12] Han Y., Biggs J. D. and Cui N., “Adaptive fault-tolerant control of spacecraft attitude dynamics with actuator failures,” Journal of Guidance, Control, and Dynamics, 2015, vol. 38, no. 10, pp. 2033-2042.
[13] Chen W. and Saif M., “Observer-based fault diagnosis of satellite systems subject to time-varying thruster faults,” 2007,
[14] Mao Z., Yan X.-G., Jiang B. and Chen M., “Adaptive fault-tolerant sliding-mode control for high-speed trains with actuator faults and uncertainties,” IEEE Transactions on Intelligent Transportation Systems, 2019, vol. 21, no. 6, pp. 2449-2460.
[15] Guo B. and Chen Y., “Adaptive fast sliding mode fault tolerant control integrated with disturbance observer for spacecraft attitude stabilization system,” ISA transactions, 2019, vol. 94, pp. 1-9.
[16] Shen Q., Wang D., Zhu S. and Poh K., “Finite-time fault-tolerant attitude stabilization for spacecraft with actuator saturation,” IEEE Transactions on Aerospace and Electronic Systems, 2015, vol. 51, no. 3, pp. 2390-2405.
[17] Ashayeri L., Doustmohammadi A. and Saberi F. F., “Fault-tolerant control of flexible satellite with infinite-dimensional model,” Advances in Space Research, 2021, vol. 68, no. 7, pp. 3080-3092.
[18] Jia Q., Chen W., Zhang Y. and Li H., “Fault reconstruction for Takagi–Sugeno fuzzy systems via learning observers,” International journal of Control, 2016, vol. 89, no. 3, pp. 564-578.
[19] Hu H., Liu L., Wang Y., Cheng Z. and Luo Q., “Active fault-tolerant attitude tracking control with adaptive gain for spacecrafts,” Aerospace Science and Technology, 2020, vol. 98, p. 105706.
[20] Liu C., Vukovich G., Sun Z. and Shi K., “Observer-based fault-tolerant attitude control for spacecraft with input delay,” Journal of Guidance, Control, and Dynamics, 2018, vol. 41, no. 9, pp. 2041-2053.
[21] Gao S., Jing Y., Dimirovski G. M. and Zheng Y., “Adaptive fuzzy fault-tolerant control for the attitude tracking of spacecraft within finite time,” Acta Astronautica, 2021, vol. 189, pp. 166-180.
[22] Bailey T. and Hubbard Jr J. E., “Distributed piezoelectric-polymer active vibration control of a cantilever beam,” Journal of Guidance, Control, and Dynamics, 1985, vol. 8, no. 5, pp. 605-611.
[23] Hu Q. and Ma G., “Spacecraft vibration suppression using variable structure output feedback control and smart materials,” 2006.
[24] Song G. and Kotejoshyer B., “Vibration reduction of flexible structures during slew operations,” International journal of Acoustics and Vibration, 2002, vol. 7, no. 2, pp. 105-109.
[25] Cao T., Gong H., Cheng P. and Xue Y., “A novel learning observer-based fault-tolerant attitude control for rigid spacecraft,” Aerospace Science and Technology, 2022, vol. 128, p. 107751.
[26] Liang X., Wang Q., Hu C. and Dong C., “Fixed-time observer based fault tolerant attitude control for reusable launch vehicle with actuator faults,” Aerospace Science and Technology, 2020, vol. 107, p. 106314.
[27] Shahravi M. and Azimi M., “Attitude and vibration control of flexible spacecraft using singular perturbation approach,” International Scholarly Research Notices, 2014, vol. 2014,
[28] Xu Y.-T., Wu A.-G., Zhu Q.-H. and Dong R.-Q., “Observer-based sliding mode control for flexible spacecraft with external disturbance,” IEEE Access, 2020, vol. 8, pp. 32477-32484.
[29] Hu Q., “Robust adaptive sliding-mode fault-tolerant control with L2-gain performance for flexible spacecraft using redundant reaction wheels,” IET control theory & applications, 2010, vol. 4, no. 6, pp. 1055-1070.
[30] Zhang L., Hua C. and Guan X., “Distributed output feedback consensus tracking prescribed performance control for a class of non‐linear multi‐agent systems with unknown disturbances,” IET Control Theory & Applications, 2016, vol. 10, no. 8, pp. 877-883.
[31] Corless M. and Leitmann G., “Continuous state feedback guaranteeing uniform ultimate boundedness for uncertain dynamic systems,” IEEE Transactions on Automatic Control, 1981, vol. 26, no., pp. 1139-1144.
[32] Azimi M., Eghlimi Dezh M. and Alikhani A., “Integral Sliding Mode Fault-Tolerant Control and Active Vibration Suppression of a Flexible Spacecraft in the Presence of External Disturbances,” Aerospace Mechanics, 2023, vol. 19, no. 1, pp. 137-151 (In persian).
[33] Feng Y., Yu X. and Man Z., “Non-singular terminal sliding mode control of rigid manipulators,” Automatica, 2002, vol. 38, no. 12, pp. 2159-2167.
[34] Zhu Z., Xia Y. and Fu M., “Attitude stabilization of rigid spacecraft with finite‐time convergence,” International Journal of Robust and Nonlinear Control, 2011, vol. 21, no. 6, pp. 686-702.
[35] Azimi M. and Sharifi G., “A hybrid control scheme for attitude and vibration suppression of a flexible spacecraft using energy-based actuators switching mechanism,” Aerospace Science and Technology, 2018, vol. 82, pp. 140-148.
[36] McDuffie J., Shtessel Y., McDuffie J. and Shtessel Y., "A sliding mode controller and observer for satellite attitude control," in Guidance, Navigation, and Control Conference, 1997, p. 3755.
