|Table of Contents|

Profile Planning for Attitude Maneuver of Flexible SpacecraftsBased on Multi-objective Optimization


Research Field:
Publishing date:


Profile Planning for Attitude Maneuver of Flexible SpacecraftsBased on Multi-objective Optimization
ZHOU Duan1SHEN Xiao-ning2GUO Yu1CHEN Qing-wei1HU Wei-li1
1. School of Automation,NUST,Nanjing 210094,China;2. School of Information andControl,Nanjing University of Information Science and Technology,Nanjing 210044,China
flexible spacecrafts attitude maneuver multi-objective optimization r-dominanceprofile planning
To solve the conflicts between rapidity and stability in the attitude maneuver control,aprofile planning and parameters optimization for the large angle maneuver of flexible spacecrafts arestudied here. Based on the dynamics analysis of flexible spacecrafts, a robust maneuver controlstrategy is designed,and a asymmetric trapezoidal speed profile is proposed. The multi-objective opti-mization model of the profile planning is constructed for the large angle rapid maneuver of flexiblespacecrafts,and an improved r-dominance multi-objective optimization algorithm for the planning isproposed to ensure the solution diversity and modify the expression of the decision maker爷spreferences. Simulation results demonstrate the effectiveness of the profile planning and the proposedoptimization method.


[1]章仁为. 卫星轨道姿态动力学与控制[M]. 北京:北京航空航天大学出版社,1998.
[2] Wang Zhi, Lang Baohua. Compound control systemdesign based on backstepping techniques and neuralnetwork sliding mode for flexible satellite [ A ].Proceedings of the 2010 International Conference onComputer Design and Applications[ C] Qinhuangdao:IEEE,2010:418-422.
[3] Rusli R, Nagarajan R, Rahim M A. Three-axis fuzzyvariable structure control with an application to microsatellite[J]. Space Science and Communication,2009:24-29.
[4] Nagashio K. Robust control of flexible mechanicalsystems by utilizing symmetry and its application tolarge space structures [ J ]. Control SystemsTechnology,2009,17(3):671-680.
[5] 高桦,邢志钢. 基于轨迹跟踪的飞行器大角度姿态机动物理仿真[ J]. 飞行器测控学报,2008,27(6):14-17.Gao Hua, Xing Zhigang. Physical simulation forspacecraft large angle maneuver based on trajectorycontrol[ J]. Journal of Spacecraft TT&C Technology,2008,27(6):14-17.
[6] 崔逊学. 多目标进化算法及其应用[M]. 北京:国防工业出版社,2006.
[7] 郑金华. 多目标进化算法及其应用[M]. 北京:科学出版社,2007.
[8] Gizem Karsli,Ozan Tekinalp. Trajectory optimization ofadvanced launch system [ A]. Recent Advances inSpace Technologies [ C]. Linguistics, Greek: IEEE,2005:374-378.
[9] 申晓宁,周端,郭毓,等. 多目标进化算法在卫星姿态控制中的应用[J]. 计算机科学,2010,37(7):248-263.Shen Xiaoning, Zhou Duan, Guo Yu, et al. Attitudecontrol for large angle maneuver of flexible satellitebased on a multi-objective evolutionary algorithm[ J].Computer Science,2010,37(7):248-263.
[10] Lamjed B S, Slim B, Khaled G. The r-Dominance: anew dominance relation for interactive evolutionarymulticriteria decision making [ J]. IEEE Trans EvolComput ,2010,14(5):801-818.
[11] 屠善澄. 卫星姿态动力学与控制[M]. 北京:中国宇航出版社,2005.
[12] 吴宏鑫,胡军,解永春. 基于特征模型的智能自适应控制[M]. 北京:中国科学技术出版社,2008.
[13] Deb K, Pratap A, Agarwal S, et al. A fast and elitistmultiobjective genetic algorithm:NAGA-域[ J]. IEEETrans Evol Comput,2002,6(2):182-197.
[14] 李英波. 挠性充液航天器动力学分析与姿态控制研究[D]. 上海: 上海交通大学机械与动力工程学院,2001.
[15] Zhou Fengqi,Lei Jing,Liu Yingying,et al. Closed-loopidentification and compensation for environmentaldisturbance torques acting on spacecraft[J]. Journal ofAstronautics,2009,30(4):1391-1395.
[16] 公茂果,焦李成,杨咚咚,等. 进化多目标优化算法研究[J]. 软件学报,2009,20(2):271-289.Gong Maoguo,Jiao Licheng,Yang Dongdong,et al. Ev-olutionary multi-objective optimization algorithms[ J].Journal of Software,2009,20(2):271-289.


Last Update: 2012-11-26