一种带大挠性附件卫星的低阶鲁棒控制方法

doi:10.3969/j.issn.1674-1579.2015.03.006

Abstract

Abstract: To deal with the flexible parameters uncertainties and external torque disturbance problems of satellites with large flexible appendages, a robust Hinfinity feedback multiinput, multioutput (MIMO) controller is proposed based on linear matrix inequalities (LMI). Parameters perturbations that caused by solar paddles rotating towards the sun and antenna’s expanding process are considered in the coupled dynamics of satellite. The proposed robust controller guarantees robust stability against the a forementioned higher vibration modes and modal parameters uncertainties for a linear parameter varying (LPV) MIMO system. Moreover, it is simple and suitable for engineering practice. The simulation results show that the given controller provides rapid stabilization for threeaxis attitude control, and is more robust than the typical PID controller in vibration and disturbance suppression.

Key words: flexible satellite, attitude control, control, LPV system, LMI

CLC Number:

HU Meng, TANG Liang. LowOrder Robust Control for Satellite with Large Flexible Appendages[J]., 2015, 41(3): 28-32.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674-1579.2015.03.006

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2015/V41/I3/28

References

［1］陈亚陵．挠性卫星姿态运动的鲁棒控制技术［J］．厦门大学学报，2001，40(2)：211219. CHEN Y L. Robust control technigue of flexible satellite attitude movement［J］. Journal of Xiamen University, 2001,40(2):211219. ［2］XIE L H, SOH Y C. Robust control of linear systems with generalized positive real uncertainty［J］. Automatica,1997,33(5):963967. ［3］CAO C U,HOVAKIMYAN N. Stability margins of L1 adaptive control architecture［J］. IEEE Transactions on Automatic Control. 2010,55(2):480487. ［4］BALLOIS S L,DUC G. H∞ control of an earth observation satellite［J］. Journal of Guidance,Control,and Dynamics,1996,19(3):628635. ［5］CHARBONNEL C. H∞ and LMI attitude control design: towards performances and robustness enhancement［J］. Acta Astronautica, 2004,54:307314. ［6］CHIAPPAM C, BODINEAU G, BOULADE S, et al.(μMμ)iteration technique: application to attitude control of satellite with large flexible appendages［C］//The 44th IEEE Conference on Decision and Control. New York: IEEE,2005：641646. ［7］倪茂林, 吴宏鑫. 线性不确定系统的鲁棒稳定控制器设计［J］. 自动化学报, 1992,18(5):585589. NI M L, WU H X. The design of a robust stabilizing controllers for uncertain systems［J］. Acta Automatica Sinica, 1992,18(5):585589. ［8］KIDA T, OHTANI T, HAMADA Y. Design and implementation of robust symmetric attitude controller for ETSVIII spacecraft［J］.Control Engineering Practice,2010,18(12):14401451. ［9］NAGASHIO T, KIDA T, OHTANI T, et al. Robust twodegreesoffreedom attitude controller design and Flight Test Result for Engineering Test SatelliteVIII Spacecraft［J］. IEEE Transactions on Control Systems Technology, 2014,22(1):157168. ［10］屠善澄.卫星姿态动力学与控制［M］.北京: 宇航出版社, 2006:245273. ［11］俞立.鲁棒控制线性矩阵不等式处理方法［M］.北京:清华大学出版社, 2002:4459.

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LowOrder Robust Control for Satellite with Large Flexible Appendages

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