一种带大挠性附件卫星的低阶鲁棒控制方法

Like

Knowledge

LowOrder Robust Control for Satellite with Large Flexible Appendages

Abstract

References

Metrics

Abstract

Cite this article

share this article

References

Related Articles 15

Metrics

Comments

Recommended 10

doi:10.3969/j.issn.1674-1579.2015.03.006

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.

0
/ Save 0 / Recommend

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

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

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

［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.

Viewed

Full text

From	Others	local

Times	2	57
Rate	3%	97%

Abstract

Just accepted	Online first	Issue

0	0	76

	From	Others

	Times	76
	Rate	100%

Cited

Web of Science	Crossref	ScienceDirect	Search for Citations in Google Scholar >>


This page requires you have already subscribed to WoS.

Shared

[1]	CAO Shengfu, YU Yuanjin, ZHAO Lei, SHI Yangyang. Parameter Perturbation Suppression Method for CMG Framework Servo System Based on H2/H∞ Composite Control [J]. Aerospace Contrd and Application, 2025, 51(1): 65-74.
[2]	ZHAN Bwen, GUO Ruike, XU Shuanfeng, WEI Chunling, ZHANG Haibo. Control Strategy of Dual Arm Robot for Peg-in-Hole Assembly Tasks [J]. Aerospace Contrd and Application, 2025, 51(1): 85-95.
[3]	ZHANG Yubo, WANG Lintao, LI Lin, WANG Xiaoming, XU Zhenbang, CHEN Yang. Low Frequency Vibration Isolator Driven by Piezoelectric Ceramics [J]. Aerospace Contrd and Application, 2025, 51(1): 25-32.
[4]	WANG Yong, LIU Tao, QIAO Dezhi, ZHENG Yongjie, LI Yi, YU Dan, HU Jinchang, MA Lin, GUO Chaoli, QIU Fang, GUI Qinhua. Guidance Navigation and Control Technology for the Autonomous Lunar Rendezvous and Docking of the Chang’e-6 Mission [J]. Aerospace Contrd and Application, 2024, 50(6): 24-33.
[5]	YU Bo, CHEN Yao, LI Xiaofeng, ZHANG Honghua, DONG Xiaogang, LI Jingsong, WANG Jiajia. Reliability Design of Chang’e-6 Control Software [J]. Aerospace Contrd and Application, 2024, 50(6): 50-56.
[6]	ZHANG Honghua, LI Ji, YU Jie, GUAN Yifeng, ZHANG Xiaowen, WANG Zhiwen, CHEN Yao, HUA Baocheng. Hazard Avoidance Techniques in Chang’e-6 Lunar Far Side Soft Landing [J]. Aerospace Contrd and Application, 2024, 50(6): 1-11.
[7]	LI Wei, LIANG Xingang, LI Fei, MA Xue. Design and Application of Separate Propulsion System for Full Electric Propulsion Satellite [J]. Aerospace Contrd and Application, 2024, 50(5): 55-61.
[8]	MA Xue, GUO Tingrong, GUO Jianxin, LIU Xiaoxiang. Station-Keeping Scheme of Electric Propulsion Geostationary Spacecraft with Double Robotic Arms [J]. Aerospace Contrd and Application, 2024, 50(5): 69-76.
[9]	LYU Nan, GUO Jianxin, XIAO Shuai, LIN Bo, ZHONG Xiaoqing, ZHOU Zhicheng. A Review on Development of Control Techniques for DFH-Series Communication Satellites [J]. Aerospace Contrd and Application, 2024, 50(5): 1-16.
[10]	LIN Baojun, LIN Xia, WANG Jingyin, LI Xiaoyue, WANG Shen, LI Shaoqian, WANG Yabin. BDS3 Satllite Attitude and Orbit Control Technology Based on Subject Chain Method [J]. Aerospace Contrd and Application, 2024, 50(5): 26-36.
[11]	CAI Chensheng, ZHU Qinghua, TANG Yucong, ZHANG Yanquan. Spacecraft Control and Simulation Technology Based on Multi Physical Field Coupling Modeling [J]. Aerospace Contrd and Application, 2024, 50(5): 84-91.
[12]	ZHANG Liang, YAN Jie, ZHANG Zhe, HUANG Panxing. Active Disturbance Rejection Control of Kinetic Energy Interceptor Based on Novel Nonlinear Function [J]. Aerospace Contrd and Application, 2024, 50(4): 55-65.
[13]	ZHOU Yuanlin, CAI Biao, LIU Zhiyong. Design of a Universal Multi-Spacecraft Collaborative Hardware-in-the-Loop (HIL) Simulation Platform of Guidance Navigation and Control System [J]. Aerospace Contrd and Application, 2024, 50(4): 66-74.
[14]	SHANG Xia, HUANG Ming, LI Bing, ZHANG Feng, LAN Baojun. Real time TT&C Scheme Geosynchronous Orbit Satellite Global Deployment [J]. Aerospace Contrd and Application, 2024, 50(3): 33-41.
[15]	GUAN Tao, LI Bin, WU Yunli. Finite Time Spacecraft Attitude Reorientation Control Under Pointing Constrains [J]. Aerospace Contrd and Application, 2024, 50(3): 52-59.

Just accepted

Online first

Just accepted

Online first