Application of Fuzzy Auto Disturbance Rejection Controller&nbsp;in Flexible Spacecraft Vibration Suppression

PDF(1812 KB)

Journal of Vibration and Shock ›› 2015, Vol. 34 ›› Issue (9) : 9-14.

Application of Fuzzy Auto Disturbance Rejection Controller in Flexible Spacecraft Vibration Suppression

Liu Fu-cai, Chen Xin, Jia Ya-fei, Liu Cai-feng

Author information +

History +

Abstract

Considering the continuous vibration of flexible structure in the on-orbit motion process of the flexible spacecraft, an auto disturbance rejection control(ADRC) strategy based on fuzzy control theory is proposed, so as to realize the vibration suppression of the flexible spacecraft. The nonlinear auto disturbance rejection controller is designed to quickly suppress the low frequency in the flexible spacecraft, and in order to improve the performance of ADRC, we combine fuzzy control to adjust the ADRC parameters easily. Compared with PID control and the nonlinear ADRC control, simulation results show that the controller can suppress the vibration of the flexible spacecraft more quickly and efficiently, and has important value for theoretical research and engineering application.

Key words

auto disturbance rejection controller / fuzzy control / vibration suppression / flexible spacecraft

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations

Liu Fu-cai, Chen Xin, Jia Ya-fei, Liu Cai-feng. Application of Fuzzy Auto Disturbance Rejection Controller in Flexible Spacecraft Vibration Suppression[J]. Journal of Vibration and Shock, 2015, 34(9): 9-14

References

[1]刘天雄, 林益明, 王明宇等. 航天器振动控制技术进展[J].宇航学报, 2008, 29(1): 1-11.
LIU Tian-xiong, LIN Yi-ming, WANG Yu. Review of the Spacecraft Vibration Control Technology[J]. Journal of Astronautics, 2008, 29(1): 1-11.
[2]Gangbing Song, Brij N. Agrawal. Vibration suppression of flexible spacecraft during attitude control[J]. Acta As- ronautica, 2001, 49(2): 73-83.
[3]Kong Xianren, Yang Zhengxian. Combined feedback control and input shaping for vibration suppression of flexible spa- cecraft[C]. Proceedings of the 2009 IEEE International Conf-
erence on Mechatronics and Automation. Changchun: IEEE, 2009,3257-3262.
[4]王晓磊, 吴宏鑫. 挠性航天器振动抑制的自适应方法及实验研究[J]. 宇航学报, 2005, 26(3): 275-291.
WANG Xiao- lei, WU Hong-xin. Adaptive control scheme and experiment for vibration suppression of flexible spacecraft[J]. Journal of Astronautics, 2005, 26(3): 275-291.
[5]孙多青. 分层模糊广义预测控制及其在挠性航天器振动抑制中的应用[J]. 宇航学报, 2009, 30(4): 1537-1543.
SUN Duo-qing. Hierarchical Fuzzy Generalized Predictive Control and Its Application in Vibration Suppression of Flexible Spacecraft. Journal of Astronautics, 2009, 30(4):1537-1543.
[6]陈涛, 胡超, 黄文虎. 航天器姿态调整时的变结构控制与振动抑制方法[J]. 宇航学报, 2007, 28(5): 1199-1204. CHEN Tao, HU Chao, HUANG Wen-hu. Variable Structure Control and Vibration Suppression of Spacecraft During Attitude Maneuver[J]. Journal of Astronautics, 2007, 28(5): 1199-1204.
[7]Hu Q L, Ma G F.Vibration suppression of flexible spacecraft during attitude maneuvers[J].J of Guidance, Control and Dynamics, 2005, 28(2): 377-380.
[8]袁国平, 史小平, 李隆. 航天器姿态机动的自适应鲁棒控制方法及主动振动抑制[J]. 振动与冲击, 2013, 32(12): 110-115.
YUAN Guo-ping, SHI Xiao-ping, LI Long. Adaptive robust attitude maneuver control of a flexible spacecraft with active vibration suppression[J]. Journal of Vibration and Shock, 2013, 32(12): 110-115.
[9]T.P. Sales, D.A. Rade, L.C.G. Souza. Passive vibration control of flexible spacecraft using shunted piezoelectric transducers[J]. Aerospace Science and Technology, 2013 (29): 403-412.
[10]M. Malekzadeh, A. Naghash, H.A. Talebi. Slewing and vibration control of a nonlinear flexible spacecraft[C]. American Control Conference, USA, 2010.
[11]孔宪仁, 杨正贤, 叶东等. 基于输入成形的柔性航天器振动闭环抑制方法研究[J]. 振动与冲击, 2010, 29(3): 72-76.
KONG Xian-ren, YANG Zheng-xian, YE Dong. Feedback control in conjunction with input shaping for flexible spacecraft vibration suppression[J]. Journal of Vibration and Shock, 2010, 29(3): 72-76.
[12]李洋, 仇原鹰, 张军等. 一种挠性航天器的自适应姿态控制与振动控制[J]. 振动与冲击, 2009, 28 (12): 178-182.
LI Yang, QIU Yuan-ying, ZHANG Jun. Adaptive attitude control and active vibration control of the flexible spacecraft[J]. Journal of Vibration and Shock, 2009, 28(12): 178-182.
[13]康莹, 李东海, 老大中. 航天器姿态的自抗扰控制与滑模控制的性能比较[J]. 控制理论与应用, 2013, 30(12): 1623-1629.
KANG Ying, LI Dong-hai, LAO Da-zhong. Performance comparison of active disturbance rejection control and sliding mode control in spacecraft attitude control[J]. Control Theory and Applications, 2013, 30(12): 1623-1629.
[14]ZHENG Q, CHEN Z Z, GAO Z Q. A practical approach to disturbance decoupling control[J]. Engineering practice, 2009, 17(9): 1016-1025.