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具有刚-柔-液-控耦合的航天器动力学研究进展

岳宝增 宋晓娟

岳宝增, 宋晓娟. 具有刚-柔-液-控耦合的航天器动力学研究进展[J]. 力学进展, 2013, 43(1): 163-173. doi: 10.6052/1000-0992-12-025
引用本文: 岳宝增, 宋晓娟. 具有刚-柔-液-控耦合的航天器动力学研究进展[J]. 力学进展, 2013, 43(1): 163-173. doi: 10.6052/1000-0992-12-025
YUE Baozeng, SONG Xiaojuan. ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT[J]. Advances in Mechanics, 2013, 43(1): 163-173. doi: 10.6052/1000-0992-12-025
Citation: YUE Baozeng, SONG Xiaojuan. ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT[J]. Advances in Mechanics, 2013, 43(1): 163-173. doi: 10.6052/1000-0992-12-025

具有刚-柔-液-控耦合的航天器动力学研究进展

doi: 10.6052/1000-0992-12-025
基金项目: 国家自然科学基金(10772026,11072030)及中国教育部博士点博士资助项目(20080070011)
详细信息
    作者简介:

    岳宝增, 男, 北京理工大学宇航学院力学系教授、博士生导师. 主要研究方向为动力学与控制(包括非线性系统动力学、液体晃动动力学及复杂航天器姿态动力学与控制), 现任全国一般力学专业委员会委员、《力学学报》特邀编委、《力学与实践》编委; 在AIAA Journal, Physical Review,Nonlinear Dynamics, Science China,《力学进展》、《力学学报》及《宇航学报》等学术刊物上发表学术论文80 多篇, SCI 检索论文20 篇、EI 检索30 多篇, 中科院出版基金资助出版专著《液体大幅晃动动力学》一部. 先后承担中国自然科学基金项目4 项、教育部博士点基金项目1 项及其他科研项目.

    通讯作者:

    岳宝增

  • 中图分类号: V412.4

ADVANCES IN RIGID-FLEXIBLE-LIQUID-CONTROL COUPLING DYNAMICS OF SPACECRAFT

Funds: The project was supported by the Natural Science Foundation of China(10772026,11072030),Ph.D.Programs Foundation of Ministry of Education of China(20080010011).
More Information
    Corresponding author: YUE Baozeng
  • 摘要: 从现代复杂航天器姿态非线性动力学、液体燃料晃动动力学与控制问题、航天器刚-柔耦合系统动力学建模问题、航天器刚-液耦合动力学、航天器刚-柔-液-控耦合动力学、充液航天器实验问题等方面概述了近年来国内外在充液航天器多体耦合动力学相关领域的最新研究进展. 分别从液体燃料晃动动力学建模问题、航天器刚-柔-液-控耦合系统非线性理论和方法、计算机数值仿真及物理实验问题等方面展望了有待进一步加强的研究课题.

     

  • 1 Marsell B, Griffin D, Schallhorn P. Integrated CFD and controls analysis interface for high accuracy liquid propellant slosh prediction. AIAA paper, 2012-0308, 2012
    2 Thomas A B. Cassini orbit trim maneuvers at Saturnoverview of attitude control flight operations. AIAA paper,2011-6549, 2011
    3 Wendy M M, Kristin L B, Oscar C, et al. Solar dynamics observatory guidance, navigation, and control system overview. AIAA paper, 2011-6726, 2011
    4 Baeten A, Juettner C. Orbit insertion dynamics of a Picosatellite with respect to coupled solid-liquid dynamics. AIAA paper, 2011-391, 2011
    5 Nathan L S, Dillon J S, Robert B, et al. Investigation to determine resonant behavior from propellant slosh in spinning on-orbit propellant storage and transfer system. AIAA paper, 2011-2000, 2011
    6 David J B, Paul A M. Method for CFD simulation of propellant sloshing in a spherical tank. AIAA paper, 2011-5681, 2011
    7 Charlot L, Etienne, Pelletier D. Verification of a free surface adaptive finite element solution algorithm. AIAA paper,2011-666, 2011
    8 屠善澄. 卫星姿态动力学与控制. 北京: 宇航出版社, 2001
    9 李青, 马兴瑞, 王天舒. 非轴对称贮箱液体晃动的等效力学模 型. 宇航学报, 2011, 32(2): 242-249
    10 黄华, 杨雷, 张熇, 等. 航天器贮箱大幅液体晃动三维质心面 等效模型研究. 宇航学报, 2010, 31(2): 55-59
    11 吴宏鑫. 基于特征模型的智能自适应控制. 北京: 中国科学 技术出版社, 2009
    12 Guan H, Xu S J. One de-orbit attitude control system coupled with liquid sloshing of residual fuel. 2011 IEEE,1137-1140
    13 王照林, 刘延柱. 充液系统动力学. 北京: 科学出版社, 2002
    14 王照林. 运动稳定性及其应用. 北京: 高等教育出版社, 1992
    15 岳宝增. 液体大幅晃动动力学. 北京: 科学出版社, 2011
    16 Yue B Z. Study on the chaotic dynamics in attitude maneuver of liquid-filled flexible spacecraft. AIAA Journal,2011, 49(10): 2090-2099  
    17 Peterson L D, Crawley E F. The nonlinear dynamics of a spacecraft coupled to the vibration of a contained fluid. AIAA, 1988-2470
    18 Disotto E, Caramago A, Mancuso S. Design and performance assessment of guidance algorithms for vision based rendezvous. AIAA paper, 2006-6586, 2006
    19 Anderson J, Turan O, Semercigil S. Experiments to control sloshing in cylindrical containers. Journal of Sound and Vibration, 2001, 240(2): 398-404  
    20 Kurode S, Bandyopadhyay B, Gandhi P S. Sliding mode control for slosh-free motion of a container using partial feedback linearization. In: International Workshop on Variable Structure Systems, Antalya, Turkey, 2008, 7:367-372
    21 Yano K, Terashima K. Robust liquid container transfer control for complete sloshing suppression. IEEE Transactions on Control System Technology, 2001, 9(3): 483-493  
    22 Sira-Ramirez H, Fliess M. A flatness based generalized PI control approach to liquid sloshing regulation in a moving container. In: Proceedings of American Control Conference.2002, (4). 2909-2914
    23 Komoguchi Y, Kunieda M, Yano K. Liquid handling control for service robot by hybrid shape approach. In: Proceedings of SICE Annual Conference, 2008. 1737-1740
    24 Yano K, Terashima K. Sloshing suppression control of liquid transfer systems considering a 3-d transfer path. In: Proceedings of IEEE/ASME Transactions on Mechatronics,2005, 20(1): 8-16
    25 Chen S J, Hein B, Worn H. Using acceleration compensation to reduce liquid surface oscillation during a high speed transfer. In: Proceedings of IEEE International Conference on Robotics and Automation, 2007. 2951-2956
    26 Dong K, Qi N M, Wang X L, et al. Dynamic influence of propellant sloshing estimation using hybrid : mechanical analogy and CFD. Trans. Japan Soc. Aero. Space, 2009,52(177): 144-151  
    27 Qi N M, Dong K, Li Y Q, et al. Hybrid approach for estimating coupling effect between propellant sloshing dynamic and spacecraft GNC. Trans. Nanjing University of Aeronautics and Astronautics, 2009, 26(2): 137-146
    28 Aboel-Hassan A, Arafa M, Nassef A. Design and optimization of input shapers for liquid slosh suppression. Journal of Sound and Vibration, 2009, 320(1-2):1-15  
    29 Pridgen B, Bai K, Singhose W. Slosh suppression by robust input shaping. In: Proceedings of 49th IEEE Conference on Decision and Control, Atlanta, USA, 2010: 2316-2321
    30 van Schoor M C. The coupled nonlinear dynamics of spacecraft with fluids in tanks of arbitrary geometry. [PhD Thesis]. Boston, USA: Massachusetts Institute of Technology,1989
    31 崔尔杰. 空天技术发展中的若干基础力学问题. 应用力学进 展. 北京: 科学出版社, 2004. 21-25
    32 吕敬. 充液挠性航天器非线性动力学研究. [博士论文]. 北 京:清华大学, 2006
    33 Modi V J. Attitude dynamics of satellites with flexible appendages-a brief review. Journal of Spacecraft and Rockets, 1974, 11(11): 746-751
    34 Nurre G S. Dynamics and control of large space structures. Journal of Guidance, Control and Dynamics, 1984, 7(5):514-526  
    35 崔赪, 王典军. 跟踪与数据中继卫星星间链路天线驱动机构 技术综述. 空间控制技术与应用, 2010, 36(5): 32-37
    36 Likins P W. Spacecraft attitude dynamics and control-a personal perspective on early developments. Journal of Guidance, Control and Dynamics, 1986, 9(2): 130-134
    37 Bainum P M. A review of modeling techniques for the open and closed loop dynamics of large space systems. In: Proceedings of 15th International Symposium on Space Technology and Science, Tokyo, Japan, AGNE Publishing, Inc., 1986. 475-482
    38 Rao S S, Pan T S, Venkayya, et al. Modeling, control, and design of flexible structure a survey. Applied Mechanics Review, 1990, 43(5): 99-117
    39 Suleman A, et al. Structural modeling issues in flexible systems. AIAA Journal, 1995, 33(5): 919-923  
    40 Shabana A A. An absolute nodal coordinates formulation for the large rotation and deformation analysis of flexible bodies. in: Mechanical Engineering, University of Illinois at Chicago, 1996
    41 Kane T R, Ryan R R, Banerjee A K. Dynamics of a cantilever beam attached to a moving base. Journal of Guidance, Control, and Dynamics, 1987, 10(2): 139-151  
    42 Banerjee A K, Kane T R. Dynamics of a plate in large overall motion. Journal of Applied Mechanics, 1989,56(11): 887-892
    43 Yoo H H, Chun G J. Dynamics of rectangular plates under going prescribed over all motion. Journal of Sound and Vibration, 2001, 239(1): 123-137  
    44 Wasfy T M, Noor A K. Computational strategies for flexible multi-body systems. Applied Mechanics Review, 2003,56(6): 553-613  
    45 Walchko K J. Robust nonlinear control with disturbance compensation. [PhD Thesis], Florida: University of Florida, 2003
    46 Pukniel A, Ja-Young K, Coverstone V L. Determination of Acquisition time and wheel control for spacecraft using a momentum transfer technique. AIAA paper 2009-6110,2009
    47 Schlapkohl T S, Ja-Young K, Coverstone V L. Analytical control law for spacecraft reorientation via Lyapunov theory. AIAA paper 2010-7894, 2010
    48 Ja-Young K, Coverstone VL. Analytical model for momentum transfer of spacecraft containing liquid. Journal of Guidance, Control, and Dynamics, 2010, 33(3):991-994  
    49 Gerrits J, Veldman A E P. Dynamics of liquid-filled spacecraft. Journal of Engineering Mathematics, 2003, 45: 21-38  
    50 Kuang J L, Meehan P A, Leung A Y T. On the chaotic rotation of a liquid-filled gyrostat via the Melnikov-HolmesMarsden integral. International Journal of Non-Linear Mechanics, 2006, 41: 475-490  
    51 Kuang J L, Meehan P A, Leung A Y T. On the chaotic instability of a nonsliding liquid-filled top with a small spheroidal base via Melnikov-Holmes-Marsden integrals. Nonlinear Dynamics, 2006, 46: 113-147  
    52 Kuang J L, Leung A Y T. Chaotic rotations of a liquidfilled solid. Journal of Sound and Vibration, 2007, 302:540-563  
    53 Hung R J, Long Y T, Chi Y M. Slosh dynamics coupled with spacecraft attitude dynamics:1.Formulation and theory. Journal of Spacecraft and Rockets, 1996, 33(4): 575-581  
    54 Hung R J, Long Y T, Chi Y M. Slosh dynamics coupled with spacecraft attitude dynamics:2.Orbital environment application. Journal of Spacecraft and Rockets, 1996,33(4): 582-593  
    55 Nichkawde C, Harish P W, Ananhkrishnan A. Stability analysis of a multi-body system model for coupled sloshvehicle dynamics. Journal of Sound and Vibration, 2004,275: 1069-1083  
    56 Sangbum C, Mcclamroch H H. Feedback control of a Space vehicle with unactuated fuel slosh dynamics. AIAA paper2000-4046, 2000
    57 Reyhanoglu M. Maneuvering control problems for a spacecraft with unactuated fuel slosh dynamics. IEEE, 2003,1: 695-699
    58 Shageer Hesham, Tao Gang. Modeling and adaptive control of spacecraft with fuel slosh: overview and case studies. AIAA paper 2007-6434, 2007
    59 Shageer Hesham, Tao Gang. Zero Dynamics Analysis for Spacecraft with Fuel Slosh. AIAA Guidance, Navigation and Control Conference and Exhibit, August 2008. 18-21
    60 Weerdt E D et al. Adaptive nonlinear dynamic inversion for spacecraft attitude control with fuel sloshing. AIAA paper 2008-7162, 2008
    61 Yang H Q, Perpeot J. Propellant sloshing parameter extraction from CFD analysis. AIAA paper 2010-6889, 2010
    62 Zhong S, Chen Y S. Bifurcation of elastic tank-liquid coupled sloshing system. Applied Mathematics and Mechanics, 2011, 32 (9): 1169-1176  
    63 Qu G J. On the development of large spacecraft Dynamics in China. ESA SP-326, 1991
    64 马兴瑞, 韩增尧, 邹元杰等. 航天器力学环境分析与条件设 计研究进展. 宇航学报, 2012, 33(1): 1-12
    65 洪嘉振, 尤超篮. 刚柔耦合系统动力学研究进展. 动力学与 控制学报, 2004, 2(2): 1-6
    66 Li Q, Wang T S, Ma X R. Geometric nonlinear effects on the planar dynamics of a pivoted flexible beam encountering a point-surface impact. Multibody System Dynamics,2009, 21: 249-260  
    67 Li Q, Wang T S, Ma X R. A note on the foreshortening effect of a flexible beam under oblique excitation. Multibody System Dynamics, 2010, 23: 209-225  
    68 田强, 张云清, 陈立平等. 柔性多体系统动力学绝对节点坐 标方法研究进展. 力学进展, 2010, 40(2): 189-202
    69 刘铖, 田强, 胡海岩. 基于绝对节点坐标的多柔性体系统动 力学高校计算方法. 力学学报, 2010, 42(6): 1198-1205
    70 Cheng L, Qiang T, Hu H Y. Dynamics and control of a spatial rigid-fleible multibody system with multiple cylindrical clearance joints. Mechanism and Machine Theory,2012, 52:106-129  
    71 胡庆雷. 挠性航天器姿态机动的主动振动控制[博士论文]. 哈尔滨: 哈尔滨工业大学, 2006
    72 Jiang Y, Hu Q L, Ma G F. Design of robust adaptive integral variable structure attitude controller with application to flexible spacecraft. International Journal of Innovative Computing, Information and Control, 2008, 4(9): 2431-2440
    73 袁长青, 李俊峰, 沈英. 多体航天器大角度机动鲁棒控制. 空 间技术与应用, 2008, 34(3): 30-36
    74 杨思亮, 徐世杰. 大角度姿态机动的变论域分形控制. 哈尔 滨工业大学学报, 2011, 43(11): 136-140
    75 Zhou L Q, Chen Y S, Chen F Q. Stability and chaos of a damped satellite partially filled with liquid. Acta Astronautica, 2009, 65: 1628-1638  
    76 杨旦旦, 岳宝增. 一类柔性附件充液航天器姿态机动控制. 力 学学报, 2012, 44(2): 415-424
    77 Zhou R, Vergalla M. Experimental methodology and numerical technique for 6-DOF tank slosh dynamics. AIAA paper 2010-6977, 2010
    78 Banerjee A K. Contribution of multi-body dynamics to space flight: a brief review. Journal of Guidance, Control, and Dynamics, 2003, 26(3): 85-394
    79 Singhose W. Command shaping for flexible systems: a review of the first 50 years. International Journal of Precision Engineering and Manufacturing, 2009, 10(4): 153-168  
    80 朱仁章. 航天交会对接技术. 北京: 国防工业出版社, 2007
    81 国家自然基金委员会(孙家广等主编). 国家自然科学基金 指南. 北京:科学出版社, 2011
    82 岳宝增, 祝乐梅. 储液罐动力学与控制研究进展. 力学进展,2011, 41(1): 45-65
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出版历程
  • 收稿日期:  2012-03-01
  • 修回日期:  2012-07-09
  • 刊出日期:  2013-01-24

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