Open Access

Attitude control for the rigid spacecraft with the improved extended state observer


Cite

[1] Gasbarri, P., R. Monti, and M. Sabatini, Very large space structures: Non-linear control and robustness to structural uncertainties. Acta Astronautica, 2014. 93: p. 252-265.Search in Google Scholar

[2] Gasbarri, P., et al., Control-oriented modelization of a satellite with large flexible appendages and use of worst-case analysis to verify robustness to model uncertainties of attitude control. Acta Astronautica, 2012. 81(1): p. 214-226.Search in Google Scholar

[3] Sattar, M. and C. Wei, Analysis of coupled torsional disturbance behavior of micro-stepped solar array drives. Journal of Sound and Vibration, 2019. 442: p. 572-597.Search in Google Scholar

[4] Iwata, T. Attitude dynamics and disturbances of the advanced land observing satellite (ALOS): modeling, identification, and mitigation. in AIAA/AAS Astrodynamics Specialist Conf. 2008.Search in Google Scholar

[5] Azadi, M., et al., Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering. Acta Astronautica, 2011. 69(5): p. 307-322.Search in Google Scholar

[6] Lu, D. and Y. Liu, Singular formalism and admissible control of spacecraft with rotating flexible solar array. Chinese Journal of Aeronautics, 2014. 27(1): p. 136-144.Search in Google Scholar

[7] Hu, Q., P. Shi, and H. Gao, Adaptive variable structure and commanding shaped vibration control of flexible spacecraft. Journal of Guidance, Control, and Dynamics, 2007. 30(3): p. 804-815.Search in Google Scholar

[8] Hu, Q., Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics. Nonlinear Dynamics, 2008. 52(3): p. 227-248.Search in Google Scholar

[9] Cao, Y., et al., Modeling for solar array drive assembly system and compensating for the rotating speed fluctuation. Aerospace Science and Technology, 2019. 84: p. 131-142.Search in Google Scholar

[10] Lu, K., et al., Sliding mode attitude tracking of rigid spacecraft with disturbances. Journal of the Franklin Institute, 2012. 349(2): p. 413-440.Search in Google Scholar

[11] Chak, Y.-C., R. Varatharajoo, and Y. Razoumny, Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system. Acta Astronautica, 2017. 133: p. 302-310.Search in Google Scholar

[12] Chen and Kun-Yung, Model Following Adaptive Sliding Mode Tracking Control Based on a Disturbance Observer for the Mechanical Systems. Journal of Dynamic Systems Measurement & Control, 2018.Search in Google Scholar

[13] Lee, D., Nonlinear disturbance observer-based robust control of attitude tracking of rigid spacecraft. Nonlinear Dynamics: p. 1-12.Search in Google Scholar

[14] De Wit, C.C. and J.-J. Slotine, Sliding observers for robot manipulators. Automatica, 1991. 27(5): p. 859-864.Search in Google Scholar

[15] Davila, J., L. Fridman, and A. Levant, Second-order sliding-mode observer for mechanical systems. IEEE transactions on automatic control, 2005. 50(11): p. 1785-1789.Search in Google Scholar

[16] Moreno, J.A. and M. Osorio. A Lyapunov approach to second-order sliding mode controllers and observers. in Decision and Control, 2008. CDC 2008. 47th IEEE Conference on. 2008. IEEE.Search in Google Scholar

[17] Moreno, J.A. and M. Osorio, Strict Lyapunov functions for the super-twisting algorithm. IEEE Transactions on Automatic Control, 2012. 57(4): p. 1035-1040.Search in Google Scholar

[18] Jingqing, H. and Z. Rong, Error analysis of the second order ESO. Journal of Systems Science and Mathematical Sciences, 1999. 19(4): p. 465-471.Search in Google Scholar

[19] Huang, Y. and J. Han. The self-stable region approach for second order nonlinear uncertain systems. in Proceedings of 1999 IFAC World Congress. 1999.Search in Google Scholar

[20] Huang, Y., A new synthesis method for uncertain systems the self-stable region approach. International journal of systems science, 1999. 30(1): p. 33-38.Search in Google Scholar

[21] Han, J., From PID to active disturbance rejection control. IEEE transactions on Industrial Electronics, 2009. 56(3): p. 900-906.Search in Google Scholar

[22] Chalanga, A., et al., Output regulation using new sliding surface with an implementation on inverted pendulum system. European Journal of Control, 2018.Search in Google Scholar

[23] Foo, G. and M. Rahman, Sensorless sliding-mode MTPA control of an IPM synchronous motor drive using a sliding-mode observer and HF signal injection. IEEE Transactions on Industrial Electronics, 2010. 57(4): p. 1270-1278.Search in Google Scholar

[24] Goforth, F.J. and Z. Gao. An active disturbance rejection control solution for hysteresis compensation. in American Control Conference, 2008. 2008. IEEE.Search in Google Scholar

[25] Gao, Z. Active disturbance rejection control: a paradigm shift in feedback control system design. in American Control Conference, 2006. 2006. IEEE.Search in Google Scholar

[26] Godbole, A.A., J.P. Kolhe, and S.E. Talole, Performance analysis of generalized extended state observer in tackling sinusoidal disturbances. IEEE Transactions on Control Systems Technology, 2013. 21(6): p. 2212-2223.Search in Google Scholar

[27] Wang, Y., Y. Yao, and K. Ma. A new type extended state observer for system with measurement noise. in 2008 IEEE International Conference on Automation and Logistics. 2008. IEEE.Search in Google Scholar

[28] Wang, Y., Y. Yao, and K. Ma. Lateral thrust and aerodynamics blended control system design based on auto disturbance-rejection controller. in 2008 IEEE International Conference on Automation and Logistics. 2008. IEEE.Search in Google Scholar

[29] Li, B., Q. Hu, and G. Ma, Extended State Observer based robust attitude control of spacecraft with input saturation. Aerospace Science and Technology, 2016. 50: p. 173-182.Search in Google Scholar

[30] Zhu, Z., et al. Attitude tracking of rigid spacecraft based on extended state observer. in Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on. 2010. IEEE.Search in Google Scholar

[31] Zhu, Z., et al., Missile guidance law based on extended state observer. IEEE Transactions on industrial Electronics, 2013. 60(12): p. 5882-5891.Search in Google Scholar

[32] Li, S., X. Yang, and D. Yang, Active disturbance rejection control for high pointing accuracy and rotation speed. Automatica, 2009. 45(8): p. 1854-1860.Search in Google Scholar

[33] Zhu, S. and Y. Lei, Disturbance analysis and feed-forward compensation for the flexible solar array sun-tracking drive. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2015. 229(14): p. 2646-2658.Search in Google Scholar

[34] Zhu, S.-y., et al., Effect of drive mechanisms on dynamic characteristics of spacecraft tracking-drive flexible systems. Journal of Sound and Vibration, 2015. 343: p. 194-215.Search in Google Scholar

[35] Shi-yao, Z., et al., Effect of drive control on dynamic characteristics of spacecraft tracking-drive flexible systems. Mechanical Systems and Signal Processing, 2021. 150: p. 107352.Search in Google Scholar

[36] Bodson, M., et al., High-performance nonlinear feedback control of a permanent magnet stepper motor. IEEE Transactions on Control Systems Technology, 1993. 1(1): p. 5-14.Search in Google Scholar

[37] Zribi, M. and J. Chiasson, Position control of a PM stepper motor by exact linearization. IEEE Transactions on Automatic Control, 1991. 36(5): p. 620-625.Search in Google Scholar

eISSN:
2444-8656
Language:
English
Publication timeframe:
Volume Open
Journal Subjects:
Life Sciences, other, Mathematics, Applied Mathematics, General Mathematics, Physics