大型卫星太阳能帆板的分布式振动控制

doi:10.7527/S1000-6893.2017.21479

固体力学与飞行器总体设计

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

大型卫星太阳能帆板的分布式振动控制

王恩美¹, 邬树楠², 王晓明¹, 吴志刚^1,2

1. 大连理工大学工业装备结构分析国家重点实验室, 大连 116024;
2. 大连理工大学航空航天学院, 大连 116024

收稿日期:2017-06-05 修回日期:2017-10-24 出版日期:2018-01-15 发布日期:2018-01-15
通讯作者: 邬树楠,E-mail:wushunan@dlut.edu.cn E-mail:wushunan@dlut.edu.cn
基金资助:
国家自然科学基金（11502040，11432010）

Distributed vibration control for large satellite solar panels

WANG Enmei¹, WU Shu'nan², WANG Xiaoming¹, WU Zhigang^1,2

1. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, China;
2. School of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024, China

Received:2017-06-05 Revised:2017-10-24 Online:2018-01-15 Published:2018-01-15
Supported by:
National Natural Science Foundation of China (11502040, 11432010)

摘要/Abstract

摘要： 针对大型卫星太阳能帆板（LSSP）振动主动控制器设计复杂、在轨扩展不易且容错性能有限等问题，提出一种适用于模块化结构的分布式振动控制方法。首先，根据LSSP的结构特点划分控制子模块，建立面向分布式控制的子模块动力学模型，并结合卡尔曼滤波算法设计各子模块线性二次最优振动控制器；然后，考虑各子模块之间的测量信息交互，提出应用于LSSP整体结构的分布式振动控制系统并分析闭环系统稳定性。最后，给出数值仿真算例以验证所提控制方法的有效性。结果表明，采用可扩展的分布式控制器，LSSP的振动能够得到有效抑制，且控制系统的容错性能良好。

关键词: 振动控制, 分布式控制, 卫星太阳能帆板, 模块化结构, 卡尔曼滤波

Abstract: To deal with the issues such as complex design, difficult on-orbit expansion, and limited fault-tolerance in active controller of vibration of Large Satellite Solar Panels (LSSP), a distributed vibration control approach, which is suitable for the modular structure, is proposed in this paper. According to the structure characteristics of the panel, the LSSP is firstly divided into different units for control system design, and the dynamic model of each unit oriented towards distributed control is developed. The linear quadratic vibration controller of each unit is then designed using the Kalman filter algorithm. Considering the communication of the measured output of each unit, the final distributed vibration control system applied to the whole LSSP is proposed, and stability of the closed-loop system is analyzed. Simulations are finally conducted to verify the validity of the proposed controllers, and the results demonstrate that scalable distributed controllers can achieve vibration suppression for LSSP, and can provide good fault tolerance.

Key words: vibration control, distributed control, satellite solar panel, modular structure, Kalman filter

中图分类号:

王恩美, 邬树楠, 王晓明, 吴志刚. 大型卫星太阳能帆板的分布式振动控制[J]. 航空学报, 2018, 39(1): 221479-221479.

WANG Enmei, WU Shu'nan, WANG Xiaoming, WU Zhigang. Distributed vibration control for large satellite solar panels[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(1): 221479-221479.

参考文献

[1] BALAS M. Trends in large space structure control theory:Fondest hopes, wildest dreams[J]. IEEE Transactions on Automatic Control, 1982, 27(3):522-535.[2] HU Q L, MA G F, LI C J. Active vibration control of a flexible plate structure using LMI-based H_∞ output feedback control law[C]//World Congress on Intelligent Control and Automation, 2004. Piscataway, NJ:IEEE Press, 2004:738-742.[3] KAR I N, MIYAKURA T, SETO K. Bending and torsional vibration control of a flexible plate structure using H_∞-based robust control law[J]. IEEE Transactions on Control Systems Technology, 2000, 8(3):545-553.[4] LUO Y J, XU M L, YAN B, et al. PD control for vibration attenuation in Hoop truss structure based on a novel piezoelectric bending actuator[J]. Journal of Sound and Vibration, 2015, 339:11-24.[5] HU Q, JIA Y H, XU S J. Adaptive suppression of linear structural vibration using control moment gyroscopes[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(3):990-996.[6] 许睿, 李东旭. 柔性太阳能帆板振动变论域自适应模糊控制[J]. 上海航天, 2012, 29(6):11-15. XU R, LI D X. Vibration control of flexible solar panel based on variable universe adaptive fuzzy control[J]. Aerospace Shanghai, 2012, 29(6):11-15(in Chinese).[7] 苗双全, 丛炳龙, 刘向东. 基于输入成形的挠性航天器自适应滑模控制[J]. 航空学报, 2013, 34(8):1906-1914. MIAO S Q, CONG B L, LIU X D. Adaptive sliding mode control of flexible spacecraft on input shaping[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(8):1906-1914(in Chinese).[8] 蒋建平, 李东旭. 智能太阳翼有限元建模与振动控制研究[J]. 动力学与控制学报, 2009, 7(2):164-170. JIANG J P, LI D X. Research of finite element modelling and vibration control for smart solar array[J]. Journal of Dynamics and Control, 2009, 7(2):164-170(in Chinese).[9] 李东旭. 大型挠性结构分散化振动控制——理论与方法[M]. 3版. 北京:科学出版社, 2013:15-16. LI D X. Decentralized vibration control of large flexible structures:Theories and methods[M]. 3rd ed. Beijing:Science Press, 2013:15-16(in Chinese).[10] 王晓明, 周文雅, 吴志刚. 压电纤维复合材料驱动的机翼动态形状控制[J]. 航空学报, 2017, 38(1):159-167. WANG X M, ZHOU W Y, WU Z G. Dynamic shape control of wings using piezoelectric fiber composite materials[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(1):159-167(in Chinese).[11] PROWALD S J, BAIER H. Advances in deployable structures and surfaces for large apertures in space[J]. CEAS Space Journal, 2013, 5(3-4):89-115.[12] 沈晓凤, 曾令斌, 靳永强, 等. 在轨组装技术研究现状与发展趋势[J]. 载人航天, 2017, 23(2):228-235. SHEN X F, ZENG L B, JIN Y Q, et al. Status and prospect of on-bit assembly technoly[J]. Manned Spaceflight, 2017, 23(2):228-235(in Chinese).[13] DORSEY J, WATSON J. Space Assembly of Large Structural System Architectures (SALSSA)[C]//AIAA SPACE 2016. Reston, VA:AIAA, 2016:1-18.[14] GARDONIO P, BIANCHI E, ELLIOTT S J. Smart panel with multiple decentralized units for the control of sound transmission. Part I:Theoretical predictions[J]. Journal of Sound and Vibration, 2004, 274(1-2):163-192.[15] GARDONIO P, BIANCHI E, ELLIOTT S J. Smart panel with multiple decentralized units for the control of sound transmission. Part Ⅱ:Design of the decentralized control units[J]. Journal of Sound and Vibration, 2004, 274(1-2):193-213.[16] GARDONIO P, BIANCHI E, ELLIOTT S J. Smart panel with multiple decentralized units for the control of sound transmission. Part Ⅲ:Control system implementation[J]. Journal of Sound and Vibration, 2004, 274(1-2):215-232.[17] LI D X, XU R. Autonomous decentralized intelligent vibration control for large split-blanket solar arrays[J]. Science China Technological Sciences, 2013, 56(3):703-712.[18] JIANG J P, LI D X. Optimal placement and decentralized robust vibration control for spacecraft smart solar panel structures[J]. Smart Materials and Structures, 2010, 19(8):085020.[19] LI D X, LIU W, JIANG J P, et al. Placement optimization of actuator and sensor and decentralized adaptive fuzzy vibration control for large space intelligent truss structure[J]. Science China Technological Sciences, 2011, 54(4):853-861.[20] QIU Z C, ZHANG X M, WU H X, et al. Optimal placement and active vibration control for piezoelectric smart flexible cantilever plate[J]. Journal of Sound and Vibration, 2007, 301(3-5):521-543.[21] NYE T W, MANNING R A, QASSIM K. Performance of active vibration control technology:The ACTEX flight experiments[J]. Smart Materials and Structures, 1999, 8(6):767-780[22] 陈亚梅. 基于形状记忆合金的太阳帆板的变结构控制[J]. 机械制造与自动化, 2009, 38(3):6-9. CHEN Y M. Variable structure control of solar panels based on shape memory alloy[J]. Machine Building and Automation, 2009, 38(3):6-9(in Chinese).[23] FAZELZADEH S A, JAFARI S M. Active control law design for flutter suppression and gust alleviation of a panel with piezoelectric actuators[J]. Smart Materials and Structures, 2008, 17(3):035013.[24] LI F M, SONG Z G. Flutter and thermal buckling control for composite laminated panels in supersonic flow[J]. Journal of Sound and Vibration, 2013, 332(22):5678-5695.[25] 檀盼龙, 孙青林, 高海涛, 等. 动力翼伞系统空投风场的辨识与应用[J]. 航空学报, 2016, 37(7):2286-2294. TAN P L, SUN Q L, GAO H T, et al. Wind identification and application of powered parafoil system[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(7):2286-2294(in Chinese).[26] 赵洲, 黄攀峰, 陈路. 一种融合卡尔曼滤波的改进时空上下文跟踪算法[J]. 航空学报, 2017, 38(2):274-284. ZHAO Z, HUANG P F, CHEN L. A tracking algorithm of improved spatio-temporal context with Kalman filter[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(2):274-284(in Chinese).[27] 段广仁. 线性系统理论[M]. 2版. 哈尔滨:哈尔滨工业大学出版社, 2004:240-246. DUAN G R. Linear systems theory[M]. 2nd ed. Harbin:Harbin Institute of Technology Press, 2004:240-246(in Chinese).[28] 秦永元, 张洪, 汪叔华. 卡尔曼滤波与组合导航原理[M]. 西安:西北工业大学出版社, 1998:20-24, 33-37. QIN Y Y, ZHANG H, WANG S H. Kalman filting and theory of integrated navigation system[M]. Xi'an:Northwestern Polytechnical University Press, 1998:20-24, 33-37(in Chinese).[29] 周舟, 陆秋海, 任革学, 等. 低密频太阳能帆板动力学参数在轨辨识和振动控制[J]. 工程力学, 2004, 21(3):84-89. ZHOU Z, LU Q H, REN G X, et al. On-orbit indentification and vibration control for solar arrays with low and close frequencies[J]. Engineering Mechanics, 2004, 21(3):84-89(in Chinese).

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

大型卫星太阳能帆板的分布式振动控制

Distributed vibration control for large satellite solar panels

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	杨加秀, 李新凯, 张宏立, 王昊. 切换拓扑下异构集群的强化学习时变编队控制[J]. 航空学报, 2024, 45(10): 329166-329166.
[2]	倪静, 马波, 杨朝旭, 陶呈纲, 周彦, 胡逸雯. 视觉/惯性着陆组合引导方法设计与试验[J]. 航空学报, 2023, 44(S1): 727636-727636.
[3]	赵祥丹, 王彪, 王志胜, 杨忠. 预测-五阶容积卡尔曼滤波方法[J]. 航空学报, 2023, 44(6): 326817-326817.
[4]	邹昕, 李明磊, 朱岱寅, 饶炜, 韩承志, 李莹. 火星降落伞开伞过程形态参数辨识与应用[J]. 航空学报, 2023, 44(6): 227007-227007.
[5]	许强, 崔洪亮, 丁邦平, 赵爱罡, 赵阳. 考虑有色噪声影响的脉冲星导航2级强跟踪差分滤波器[J]. 航空学报, 2023, 44(3): 526120-526120.
[6]	熊凯, 魏春岭, 李连升, 周鹏. 基于扩维QLEKF的脉冲星/星间定向组合导航[J]. 航空学报, 2023, 44(3): 526232-526232.
[7]	印俊秋, 刘云鹏, 汤晓斌. 基于仿脉冲星X射线信标的航天器定位方法[J]. 航空学报, 2023, 44(3): 526596-526596.
[8]	周泽波, 张泽亮, 彭鑫, 李滚, 陶洋, 王亮权, 罗鑫. 基于记忆融合模式的多无人机分散式协同导航方法[J]. 航空学报, 2023, 44(20): 628440-628440.
[9]	魏志强, 翁哲鸣, 化永朝, 董希旺, 任章. 切换拓扑下异构无人集群编队-合围跟踪控制[J]. 航空学报, 2023, 44(2): 326504-326504.
[10]	刘锬韬, 李瑞宇, 高丽敏, 赵磊. 基于数据同化的试验数据驱动的叶栅流场预测[J]. 航空学报, 2023, 44(14): 628201-628201.
[11]	赵万里, 郭迎清, 徐柯杰, 王灿森, 应豪杰, 陶欣昕. 航空发动机多电分布式控制系统故障诊断与容错关键技术综述[J]. 航空学报, 2023, 44(10): 27519-027519.
[12]	陈林秀, 杨翔宇, 张航, 赵佳佳, 郝明瑞. 基于主动雷达/红外信息融合的复合制导方法[J]. 航空学报, 2022, 43(S1): 727058-727058.
[13]	曾开春, 寇西平, 杨兴华, 余立, 查俊. 跨声速风洞试验模型主动减振结构优化设计[J]. 航空学报, 2022, 43(2): 224944-224944.
[14]	方安然, 李旦, 张建秋. 异常值和未知观测噪声鲁棒的非线性滤波器[J]. 航空学报, 2021, 42(7): 324675-324675.
[15]	段登燕, 裴家涛, 祖瑞, 李建波. 电机-变距螺旋桨动力系统功率优化控制[J]. 航空学报, 2021, 42(3): 623933-623933.