Fully actuated system approach for spacecraft rendezvous system with actuator saturation

References

• Carter, T. E. (1998). State transition matrices for terminal rendezvous studies: Brief survey and new example. Journal of Guidance Control and Dynamics, 21(1), 148–155. https://doi.org/10.2514/2.4211
   Web of Science ®Google Scholar
• Clohessy, W. H., & Wiltshire, R. S. (1960). Terminal guidance system for satellite rendezvous. Journal of the Astronautical Sciences, 27(9), 653–658.
   Web of Science ®Google Scholar
• Di Cairano, S., Park, H., & Kolmanovsky, I. (2012). Model predictive control approach for guidance of spacecraft rendezvous and proximity maneuvering. International Journal of Robust and Nonlinear Control, 22(12), 1398–1427. https://doi.org/10.1002/rnc.v22.12
   Web of Science ®Google Scholar
• Duan, G. R. (2014a). Cooperative spacecraft rendezvous–a direct parametric control approach. In Proceedings of the 11th World Congress on Intelligent Control and Automation (pp. 4589–4595). Institute of Electrical and Electronics Engineers Inc.
   Google Scholar
• Duan, G. R. (2014b). Direct parametric control of fully-actuated second-order nonlinear systems-The normal case. In Proceedings of the 33rd Chinese Control Conference (pp. 28–30). IEEE Computer Society.
   Google Scholar
• Duan, G. R. (2020). High-order system approaches – I. Fully-actuated systems and parametric designs. Acta Automatica Sinica, 46(7), 1333–1345.
   Google Scholar
• Duan, G. R. (2021). High-order fully actuated system approaches: Part III. Robust control and high-order backstepping. International Journal of Systems Science, 52(5), 952–971. https://doi.org/10.1080/00207721.2020.1849863
   Web of Science ®Google Scholar
• Duan, G. R. (2022). High-order fully actuated system approaches: Part VIII. Optimal control with application in spacecraft attitude stabilisation. International Journal of Systems Science, 53(1), 54–73. https://doi.org/10.1080/00207721.2021.1937750
   Web of Science ®Google Scholar
• Duan, G. R., & Liu, G. P. (2022). Attitude and orbit optimal control of combined spacecraft via a fully-actuated system approach. Journal of Systems Science and Complexity, 35(2), 623–640. https://doi.org/10.1007/s11424-022-1492-y
   Web of Science ®Google Scholar
• Gao, H. J., Yang, X. B., & Shi, P. (2009). Multi-objective robust H∞ control of spacecraft rendezvous. IEEE Transactions on Control Systems Technology, 17(4), 794–802. https://doi.org/10.1109/TCST.2008.2012166
   Web of Science ®Google Scholar
• Hao, Y., Lin, Z. X., Su, Z. Y., Xiao, Y. F., & Huang, B. (2022). Robust adaptive control for spacecraft rendezvous with predefined-time prescribed performance and input saturation. Journal of Aerospace Engineering, 35(1), 06021007. https://doi.org/10.1061/(ASCE)AS.1943-5525.0001353
   Web of Science ®Google Scholar
• Hu, T. S., & Lin, Z. L. (2001). Control systems with actuator saturation: Analysis and design. Birkhauser.
   Google Scholar
• Li, Q., Sun, C., Song, S., Gou, Q. X., & Niu, Z. Q. (2021). Robust adaptive control for spacecraft final proximity maneuvers with safety constraint and input quantization. ISA Transactions, 111, 35–46. https://doi.org/10.1016/j.isatra.2020.10.064
   PubMed Web of Science ®Google Scholar
• Li, Q., Yuan, J. P., & Zhang, B. (2019). Extended state observer based output control for spacecraft rendezvous and docking with actuator saturation. ISA Transactions, 88, 37–49. https://doi.org/10.1016/j.isatra.2018.11.048
   PubMed Web of Science ®Google Scholar
• Selim, A., & Ozkol, I. (2023). Real-time optimal control of a 6-DOF state-constrained close-proximity rendezvous mission. Acta Astronautica, 211, 280–294. https://doi.org/10.1016/j.actaastro.2023.06.008
   Web of Science ®Google Scholar
• Sheng, J., Geng, Y. H., Li, M., & Zhu, B. L. (2023). Finite-time contractive control of spacecraft rendezvous system. Mathematics, 11(8), 1871. https://doi.org/10.3390/math11081871
   Web of Science ®Google Scholar
• Sun, L., Huo, W., & Jiao, Z. X. (2017). Adaptive backstepping control of spacecraft rendezvous and proximity operations with input saturation and full-state constraint. IEEE Transactions on Industrial Electronics, 64(1), 480–492. https://doi.org/10.1109/TIE.2016.2609399
   Web of Science ®Google Scholar
• Sun, L., Huo, W., & Jiao, Z. X. (2018). Disturbance-observer-based robust relative pose control for spacecraft rendezvous and proximity operations under input saturation. IEEE Transactions on Aerospace and Electronic Systems, 54(4), 1605–1617. https://doi.org/10.1109/TAES.7
   Web of Science ®Google Scholar
• Wang, N., Liu, X. P., Liu, C. E., Wang, H. Q., & Zhou, Y. C. (2023). Adaptive control and almost disturbance decoupling for uncertain HOFA nonlinear systems. International Journal of Adaptive Control and Signal Processing, 37(8), 2133–2161. https://doi.org/10.1002/acs.v37.8
   Web of Science ®Google Scholar
• Wang, Q., Wu, Z. G., Shi, P., Yan, H. C., & Chen, Y. (2020). Stability analysis and control for switched system with bounded actuators. IEEE Transactions on Systems, Man, and Cybernetics: Systems, 50(11), 4506–4512. https://doi.org/10.1109/TSMC.6221021
   Web of Science ®Google Scholar
• Wang, Q., Yang, Y. T., Tian, F. J., & Chen, G. D. (2023). Event-triggered H∞ control for discrete-time switched systems with saturation nonlinearities. ISA Transactions, https://doi.org/10.1016/j.isatra.2023.11.014.
   Web of Science ®Google Scholar
• Wang, Q., Yu, H. Y., Wu, Z. G., & Chen, G. D. (2021). Stability analysis for input saturated discrete-time switched systems with average dwell-time. IEEE Transactions on Systems, Man, and Cybernetics: Systems, 51(1), 412–419. https://doi.org/10.1109/TSMC.6221021
   Web of Science ®Google Scholar
• Xia, K. W., & Zou, Y. (2021). Adaptive saturated fault-tolerant control for spacecraft rendezvous with redundancy thrusters. IEEE Transactions on Control Systems Technology, 29(2), 502–513. https://doi.org/10.1109/TCST.87
   Web of Science ®Google Scholar
• Xiao, F. Z., & Chen, L. Q. (2022). Attitude control of spherical liquid-filled spacecraft based on high-order fully actuated system approaches. Journal of Systems Science and Complexity, 35(2), 471–480. https://doi.org/10.1007/s11424-022-2055-y
   Web of Science ®Google Scholar
• Zhang, D. W., & Liu, G. P. (2023). Predictive control for networked high-order fully actuated systems subject to communication delays and external disturbances. ISA Transactions, 139, 425–435. https://doi.org/10.1016/j.isatra.2023.03.041
   PubMed Web of Science ®Google Scholar
• Zhang, K., Zhou, B., & Duan, G. R. (2022). Event-triggered and self-triggered control of discrete-time systems with input constraints. IEEE Transactions on Systems, Man, and Cybernetics: Systems, 52(3), 1948–1957. https://doi.org/10.1109/TSMC.2020.3035037
   Web of Science ®Google Scholar
• Zhang, Y. C., Ma, M. C., Yang, X. Y., & Song, S. M. (2023). Disturbance-observer-based fixed-time control for 6-DOF spacecraft rendezvous and docking operations under full-state constraints. Acta Astronautica, 205, 225–238. https://doi.org/10.1016/j.actaastro.2023.02.005
   Web of Science ®Google Scholar
• Zhang, Y. C., Wu, G. Q., Yuan, J., Yang, X. Y., & Song, S. M. (2023). Composite neural learning based appointed-time safe approach control under full-state constraints. Advances in Space Research, 72(4), 1412–1430. https://doi.org/10.1016/j.asr.2023.04.008
   Web of Science ®Google Scholar
• Zhang, Y. Q., Zhu, B. L., Cheng, M., & Li, S. L. (2022). Trajectory optimization for spacecraft autonomous rendezvous and docking with compound state-triggered constraints. Aerospace Science and Technology, 127, 107733. https://doi.org/10.1016/j.ast.2022.107733
   Web of Science ®Google Scholar
• Zhao, Q., & Duan, G. R. (2022). Fully actuated system approach for 6DOF spacecraft control based on extended state observer. Journal of Systems Science and Complexity, 35(2), 604–622. https://doi.org/10.1007/s11424-022-1498-5
   Web of Science ®Google Scholar
• Zhao, T. Y., & Duan, G. R. (2022). Fully actuated system approach to attitude control of flexible spacecraft with nonlinear time-varying inertia. Science China Information Sciences, 65(11), 212201. https://doi.org/10.1007/s11432-021-3349-3
   Web of Science ®Google Scholar
• Zhao, X. T., & Zhang, S. J. (2021). Adaptive saturated control for spacecraft rendezvous and docking under motion constraints. Aerospace Science and Technology, 114, 106739. https://doi.org/10.1016/j.ast.2021.106739
   Web of Science ®Google Scholar
• Zhao, Y. Z., Ma, D., & Ma, H. W. (2022). Adaptive neural network control of thermoacoustic instability in rijke tube: A fully actuated system approach. Journal of Systems Science and Complexity, 35(2), 386–603.
   Web of Science ®Google Scholar
• Zhou, B. (2020). Finite-time stabilization of linear systems by bounded linear time-varying feedback. Automatica, 113, 108760. https://doi.org/10.1016/j.automatica.2019.108760
   Web of Science ®Google Scholar
• Zhou, B., & Lam, J. (2017). Global stabilization of linearized spacecraft rendezvous system by saturated linear feedback. IEEE Transactions on Control Systems Technology, 25(6), 2185–2193. https://doi.org/10.1109/TCST.2016.2632529
   Web of Science ®Google Scholar
• Zhou, B., Michiels, W., & Chen, J. (2022). Fixed-time stabilization of linear delay systems by smooth periodic delayed feedback. IEEE Transactions on Automatic Control, 67(2), 557–573. https://doi.org/10.1109/TAC.2021.3051262
   Web of Science ®Google Scholar
• Zhou, B., Zhang, K. K., & Jiang, H. Y. (2023). Prescribed-time control of perturbed nonholonomic systems by time-varying feedback. Automatica, 155, 111125. https://doi.org/10.1016/j.automatica.2023.111125
   Web of Science ®Google Scholar
• Zhou, B., Zhang, Z., & Michiels, W. (2024). Functional and dual observer based prescribed time control of linear systems by periodic delayed feedback. Automatica, 159, 111406. https://doi.org/10.1016/j.automatica.2023.111406
   Web of Science ®Google Scholar