Optimal Guaranteed Cost Control of Spacecraft Large Angle Attitude Maneuvers

被引：0

作者：

Ma Qingliang ^{[1
]}

Yang Haiyan ^{[1
]}

Yue Ruihua ^{[1
]}

Cao Xiangyu ^{[1
]}

机构：

[1] Second Artillery Engn Univ, Dept Automat, Xian 710025, Peoples R China

来源：

PROCEEDINGS OF THE 31ST CHINESE CONTROL CONFERENCE | 2012年

关键词：

Guaranteed cost control; attitude control; large angle attitude maneuver; sum-of-squares optimization;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

A novel approach to guaranteed cost control of spacecraft large angle attitude maneuvers is proposed based on sum of squares (SOS) optimization. By using modified Rodrigues parameters, the attitude dynamics of the spacecraft is represented in terms of linear parameter varying (LPV) systems. Based on the analysis of system performance, a sufficient condition for the existence of state feedback guaranteed cost controller is derived by using Lyapunov approach and SOS optimization. Furthermore, the optimal guaranteed cost controller design problem is converted into a parameter optimization problem with SOS constraints. Simulation results of certain satellite attitude maneuvers demonstrate the effectiveness of the proposed design approach.

引用

页码：2307 / 2311

页数：5

共 7 条

[1]

Gollu Narendra, 2007, 2007 American Control Conference, P3156, DOI 10.1109/ACC.2007.4283054

[2]

Kim K. S., 2005, IEEE T CONTR SYST T, V13, P907

[3]

Parrilo P., 2000, Technical report

[4]

Prajna S, 2002, IEEE DECIS CONTR P, P741, DOI 10.1109/CDC.2002.1184594

[5]

Prajna S., 2004, 2004 5th Asian Control Conference (IEEE Cat. No.04EX904), P157

[6] Optimal nonlinear tracking of spacecraft attitude maneuvers [J].

Sharma, R ;

Tewari, A .

IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2004, 12 (05) :677-682

[7] Nonlinear H∞ Control Designs with Axisymmetric Spacecraft Control [J].

Zheng, Qian ;

Wu, Fen .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2009, 32 (03) :850-859

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