Finite-time attitude quantised control for rigid spacecraft

References

• Abdelrahman, M., & Park, S. Y. (2013). Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzy approach. Aerospace Science and Technology, 26(1), 16–28. doi: 10.1016/j.ast.2012.02.010
   Web of Science ®Google Scholar
• Bhat, S. P., & Bernstein, D. S. (1997). Finite-time stability of homogeneous systems. In Proceedings of the 1997 American Control Conference (Vol. 4, pp. 2513–2514). Albuquerque, NM: IEEE.
   Google Scholar
• Bhat, S. P., & Bernstein, D. S. (1998). Continuous finite-time stabilization of the translational and rotational double integrators. IEEE Transactions on Automatic Control, 43(5), 678–682. doi: 10.1109/9.668834
   Web of Science ®Google Scholar
• Cong, B., Liu, X., & Chen, Z. (2013). Backstepping based adaptive sliding mode control for spacecraft attitude maneuvers. Aerospace Science and Technology, 30(1), 1–7. doi: 10.1016/j.ast.2013.05.005
   Web of Science ®Google Scholar
• Coutinho, D. F., Fu, M., & de Souza, C. E. (2010). Input and output quantized feedback linear systems. IEEE Transactions on Automatic Control, 55(3), 761–766. doi: 10.1109/TAC.2010.2040497
   Web of Science ®Google Scholar
• Deng, C., & Yang, G.-H. (2017). Distributed adaptive consensus for linear multi-agent systems with quantised information. International Journal of Systems Science, 48(15), 3129–3137. doi: 10.1080/00207721.2017.1381282
   Web of Science ®Google Scholar
• De Persis, C., & Mazenc, F. (2010). Stability of quantized time-delay nonlinear systems: A Lyapunov–Krasowskii-functional approach. Mathematics of Control, Signals, and Systems, 21(4), 337–370. doi: 10.1007/s00498-010-0048-1
   Web of Science ®Google Scholar
• Ding, S., & Li, S. (2009). Stabilization of the attitude of a rigid spacecraft with external disturbances using finite-time control techniques. Aerospace Science and Technology, 13(4-5), 256–265. doi: 10.1016/j.ast.2009.05.001
   Web of Science ®Google Scholar
• Elia, N., & Mitter, S. K. (2001). Stabilization of linear systems with limited information. IEEE Transactions on Automatic Control, 46(9), 1384–1400. doi: 10.1109/9.948466
   Web of Science ®Google Scholar
• Fu, M., & Xie, L. (2009). Finite-level quantized feedback control for linear systems. IEEE Transactions on Automatic Control, 54(5), 1165–1170. doi: 10.1109/TAC.2009.2017815
   Web of Science ®Google Scholar
• Gao, H., & Chen, T. (2008). A new approach to quantized feedback control systems. Automatica, 44(2), 534–542. doi: 10.1016/j.automatica.2007.06.015
   Web of Science ®Google Scholar
• Hardy, G. H., Littlewood, J. E., & Pólya, G. (1952). Inequalities. Cambridge, UK: Cambridge University Press.
   Google Scholar
• Hayakawa, T., Ishii, H., & Tsumura, K. (2009). Adaptive quantized control for nonlinear uncertain systems. Systems & Control Letters, 58(9), 625–632. doi: 10.1016/j.sysconle.2008.12.007
   Web of Science ®Google Scholar
• Hu, Q., Li, B., & Qi, J. (2014). Disturbance observer based finite-time attitude control for rigid spacecraft under input saturation. Aerospace Science and Technology, 39, 13–21. doi: 10.1016/j.ast.2014.08.009
   Web of Science ®Google Scholar
• Jiang, B., Li, C., & Ma, G. (2017). Finite-time output feedback attitude control for spacecraft using “adding a power integrator” technique. Aerospace Science and Technology, 66, 342–354. doi: 10.1016/j.ast.2017.03.026
   Web of Science ®Google Scholar
• Jin, E., & Sun, Z. (2008). Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control. Aerospace Science and Technology, 12(4), 324–330. doi: 10.1016/j.ast.2007.08.001
   Web of Science ®Google Scholar
• Li, S., Wang, Z., & Fei, S. (2011). Comments on the paper: Robust controllers design with finite time convergence for rigid spacecraft attitude tracking control. Aerospace Science and Technology, 15(3), 193–195. doi: 10.1016/j.ast.2010.11.005
   Web of Science ®Google Scholar
• Liberzon, D., & Hespanha, J. P. (2005). Stabilization of nonlinear systems with limited information feedback. IEEE Transactions on Automatic Control, 50(6), 910–915. doi: 10.1109/TAC.2005.849258
   Web of Science ®Google Scholar
• Lu, R., Cheng, H., & Bai, J. (2015). Fuzzy-model-based quantized guaranteed cost control of nonlinear networked systems. IEEE Transactions on Fuzzy Systems, 23(3), 567–575. doi: 10.1109/TFUZZ.2014.2317515
   Web of Science ®Google Scholar
• Lu, R., Wu, F., & Xue, A. (2014). Networked control with reset quantized state based on Bernoulli processing. IEEE Transactions on Industrial Electronics, 61(9), 4838–4846. doi: 10.1109/TIE.2013.2289870
   Web of Science ®Google Scholar
• Lu, K., Xia, Y., Zhu, Z., & Basin, M. V. (2012). Sliding mode attitude tracking of rigid spacecraft with disturbances. Journal of the Franklin Institute, 349(2), 413–440. doi: 10.1016/j.jfranklin.2011.07.019
   Web of Science ®Google Scholar
• Lv, Y., Hu, Q., Ma, G., & Zhou, J. (2011). 6 DOF synchronized control for spacecraft formation flying with input constraint and parameter uncertainties. ISA Transactions, 50(4), 573–580. doi: 10.1016/j.isatra.2011.04.001
   PubMed Web of Science ®Google Scholar
• Park, Y. (2005). Robust and optimal attitude stabilization of spacecraft with external disturbances. Aerospace Science and Technology, 9(3), 253–259. doi: 10.1016/j.ast.2005.01.002
   Web of Science ®Google Scholar
• Ruiter, A. H. J. D. (2012). Adaptive spacecraft attitude control with actuator saturation. Journal of Guidance Control and Dynamics, 33(5), 1692–1696. doi: 10.2514/1.46404
   Web of Science ®Google Scholar
• Sabanovic, A. (2011). Variable structure systems with sliding modes in motion control – A survey. IEEE Transactions on Industrial Informatics, 7(2), 212–223. doi: 10.1109/TII.2011.2123907
   Web of Science ®Google Scholar
• Scarciotti, G., & Astolfi, A. (2014). Approximate finite-horizon optimal control for input-affine nonlinear systems with input constraints. Journal of Control and Decision, 1(2), 149–165. doi: 10.1080/23307706.2014.899110
   Google Scholar
• Shi, P., Wang, H., & Lim, C.-C. (2016). Network-based event-triggered control for singular systems with quantizations. IEEE Transactions on Industrial Electronics, 63(2), 1230–1238. doi: 10.1109/TIE.2015.2475515
   Web of Science ®Google Scholar
• Shi, X. N., Zhou, Z. G., & Zhou, D. (2017). Global finite-time attitude stabilization for rigid spacecraft in the exponential coordinates. International Journal of Control, 91(6), 1325–1337. doi: 10.1080/00207179.2017.1314020
   Web of Science ®Google Scholar
• Shuster, M. D. (1993). A survey of attitude representations. Navigation, 8(9), 439–517.
   Google Scholar
• Song, Z., Li, H., & Sun, K. (2014). Finite-time control for nonlinear spacecraft attitude based on terminal sliding mode technique. Isa Transactions, 53(1), 117–124. doi: 10.1016/j.isatra.2013.08.008
   PubMed Web of Science ®Google Scholar
• Wang, Y., Shen, H., & Duan, D. (2017). On stabilization of quantized sampled-data neural-network-based control systems. IEEE Transactions on Cybernetics, 47(10), 3124–3135. doi: 10.1109/TCYB.2016.2581220
   PubMed Web of Science ®Google Scholar
• Wu, B. (2015). Spacecraft attitude control with input quantization. Journal of Guidance Control and Dynamics, 39, 1–5.
   Web of Science ®Google Scholar
• Xia, Y., Yan, J., Shi, P., & Fu, M. (2013). Stability analysis of discrete-time systems with quantized feedback and measurements. IEEE Transactions on Industrial Informatics, 9(1), 313–324. doi: 10.1109/TII.2012.2218113
   Web of Science ®Google Scholar
• Xia, Y., Zhu, Z., Fu, M., & Wang, S. (2011). Attitude tracking of rigid spacecraft with bounded disturbances. IEEE Transactions on Industrial Electronics, 58(2), 647–659. doi: 10.1109/TIE.2010.2046611
   Web of Science ®Google Scholar
• Xiao, B., Hu, Q., & Friswell, M. I. (2011). Robust fault tolerant control for spacecraft attitude stabilization under actuator faults and bounded disturbance. Journal of Dynamic Systems, Measurement, and Control, 133(5), 051006. doi: 10.1115/1.4004061
   Web of Science ®Google Scholar
• Xing, G. Q., & Parvez, S. A. (2001). Nonlinear attitude state tracking control for spacecraft. Journal of Guidance, Control, and Dynamics, 24(3), 624–626. doi: 10.2514/2.4754
   Web of Science ®Google Scholar
• Xing, L., Wen, C., Zhu, Y., Su, H., & Liu, Z. (2016). Output feedback control for uncertain nonlinear systems with input quantization. Automatica, 65(C), 191–202. doi: 10.1016/j.automatica.2015.11.028
   Web of Science ®Google Scholar
• You, K., Su, W., Fu, M., & Xie, L. (2011). Attainability of the minimum data rate for stabilization of linear systems via logarithmic quantization. Automatica, 47(1), 170–176. doi: 10.1016/j.automatica.2010.10.024
   Web of Science ®Google Scholar
• Yu, S., Yu, X., Shirinzadeh, B., & Man, Z. (2005). Continuous finite-time control for robotic manipulators with terminal sliding mode. Automatica, 41(11), 1957–1964. doi: 10.1016/j.automatica.2005.07.001
   Web of Science ®Google Scholar
• Zhou, J., Wen, C., & Yang, G. (2014). Adaptive backstepping stabilization of nonlinear uncertain systems with quantized input signal. IEEE Transactions on Automatic Control, 59(2), 460–464. doi: 10.1109/TAC.2013.2270870
   Web of Science ®Google Scholar
• Zhu, B., Zhang, Z., Zhou, D., Ma, J., & Li, S. (2017). Prediction-based sampled-data H∞ controller design for attitude stabilisation of a rigid spacecraft with disturbances. International Journal of Systems Science, 48(11), 2356–2367. doi: 10.1080/00207721.2017.1316883
   Web of Science ®Google Scholar
• Zou, A. M. (2013). Finite-time output feedback attitude tracking control for rigid spacecraft. IEEE Transactions on Control Systems Technology, 22(1), 338–345. doi: 10.1109/TCST.2013.2246836
   Web of Science ®Google Scholar