Volume 46 Issue 1
May  2016
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MENG Guang, ZHOU Xubin, MIAO Jun. Mechanical problems in momentous projects of aerospace engineering[J]. Advances in Mechanics, 2016, 46(1): 201606. doi: 10.6052/1000-0992-15-018
Citation: MENG Guang, ZHOU Xubin, MIAO Jun. Mechanical problems in momentous projects of aerospace engineering[J]. Advances in Mechanics, 2016, 46(1): 201606. doi: 10.6052/1000-0992-15-018

Mechanical problems in momentous projects of aerospace engineering

doi: 10.6052/1000-0992-15-018
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  • Corresponding author: MENG Guang
  • Received Date: 2015-04-27
  • Rev Recd Date: 2016-01-04
  • Publish Date: 2016-05-20
  • With the vigorous development of the momentous projects in aerospace en-gineering field, new mechanical problems emerge continuously. Therefore, the research on engineering mechanics plays a prominent role in the developments of the space technol-ogy. The launch and operation environment for spacecraft is becoming more stringent as the spacecraft nowadays is developing on the track of super high speeds, deep space explo-ration and multifunction. Large-area and large flexible structure equipped on the spacecraft has proposed new challenges on the dynamics of deployment in orbit, modal identification and rigid-flexible coupling dynamics. Meanwhile, high-precision and high-resolution earth-observing request leads to new problems of micro-vibration control and thermally induced vibration control in orbit. All these problems urge more accurate methods for ground sim-ulations and experiments. In this paper, we outline the new mechanical problems arising from the launch of spacecraft, in orbit operation, ground simulations and experiments, etc. We focus on coupled dynamics, aerodynamics, multi-body dynamics, structure dynamics and experimental mechanics. The new problems and development directions of engineering mechanics are discussed in the end.

     

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  • [1]
    陈昌亚, 宋汉文. 2005. 卫星结构振动试验中的力控技术. 上海航天, 5: 47-53 (Chen C Y, Song H W. 2005. The technology about force limited in satellite structure vibration testing. Aerospace Shanghai, 5: 47-53).
    [2]
    陈劲松, 曹军. 1990. 超声速和高超声速翼型非定长气动力的一种近似计算方法. 空气动力学学报, 8: 339-344 (Chen J S, Cao J. 1990. An approximate calculating method of supersonic/hypersonic unsteady aerodynamic forces of airfoils. Acta Aerodynamica Sinica, 8: 339-344).
    [3]
    陈克安. 2003. 有源噪声控制. 北京: 国防工业出版社(Chen K A. 2003. Active Noise Control. Beijing: National Defence Industry Press).
    [4]
    陈珅艳, 黄海. 2011. 基于二级多点逼近算法的航天器结构优化设计. 北京航空航天大学学报, 37: 237-240 (Chen K Y, Huang H. 2011. Structural optimization of spacecraft based on two-level multi-point approximate method. Journal of Beijing University of Aeronautics and Astronautics, 37: 237-240).
    [5]
    崔尔杰. 2006. 重大研究计划"空天飞行器的若干重大基础问题" 研究进展. 中国科学基金, 5: 278-280 (Cui E J. 2006. Progress on NSFC major research plan "some key fundamental problems of aerospaceflying vehicles". Bulletin of National Natural Science Foundation of China, 5: 278-280).
    [6]
    崔尔杰. 2009. 近空间飞行器研究发展现状及关键技术问题. 力学进展, 39: 658-673 (Cui E J. 2009. Research statutes, development trends and key technical problems of near space flying vehicles. Advances in Mechanics, 39: 658-673).
    [7]
    丁亮, 高海波, 邓宗全等. 2009. 基于应力分布的月球车轮地相互作用地面力学模型. 机械工程学报, 45: 49-55 (Ding L, Gao H B, Deng Z Q, et al. 2009. Terramechanics model for wheel-terrain interaction of lunar rover based on stress distribution. Journal of Mechanical Engineering, 45: 49-55).
    [8]
    方宝东, 李应典, 张建刚. 2006. 新一代地球同步轨道气象卫星结构热变形分析. 上海航天, 6: 50-52 (Fang B D, Li Y D, Zhang J G. 2006. Thermal structure distortion for some new GEO meteorological satellite. Aerospace Shanghai, 6: 50-52).
    [9]
    盖晓男. 2013. 高速飞行器动载荷识别研究. 哈尔滨: 哈尔滨工业大学(Gai X N. 2013. Research on identification of dynamic load of high speed vehicle. Harbin: Harbin Institute of Technology).
    [10]
    葛东明, 邹元杰, 张志娟, 王泽宇. 2012. 基于全柔性卫星模型的控制闭环微振动建模与仿真. 航天器工程, 21: 58-63 (Ge D M, Zou Y J, Zhang Z J, Wang Z Y. 2012. Control closed-loop micro-vibration modeling and simulation based on flexible satellite model. Spacecraft Engineering, 21: 58-63).
    [11]
    顾松年, 徐斌, 荣见华, 姜节胜. 2005. 结构动力学设计优化方法的新进展. 机械强度, 27: 156-162 (Gu S N, Xu B, Rong J H, Jiang J S. 2005. Recent progresses on structural dynamic design methods. Journal of Mechanical Strength, 27: 156-162).
    [12]
    顾元宪, 亢战, 赵国忠, 迟军, 林益明, 白光明. 2003. 卫星承力筒复合材料结构的优化设计. 宇航学报, 24: 88-91 (Gu Y X, Kang Z, Zhao G Z, Chi J, Lin Y M, Bai G M. 2003. Optimal design of composite structure of satellite bearing cylinder. Journal of Astronautics, 24: 88-91).
    [13]
    关广丰. 2007. 液压驱动六自由度振动试验系统控制策略研究. 哈尔滨: 哈尔滨工业大学(Guan G F. 2007. Control strategy of hydraulically driven 6-DOF vibration test system. Harbin: Harbin Institute of Technology).
    [14]
    关新, 王全武, 郑钢铁. 2010. 飞轮拟主动隔振方法. 宇航学报, 31: 1870-1876 (Guan X,Wang Q W, Zheng G T. 2010. A pseudo-active vibration isolation method for reaction wheels. Journal of Astronautics, 31: 1870-1876).
    [15]
    关英姿, 崔乃刚, 刘育华. 1999. 空间飞行器对接动力学的数值仿真研究. 哈尔滨工业大学学报, 31: 121-124 (Guan Y Z, Cui N G, Liu Y H. 1999. Numerical simulation of spacecraft docking dynamics. Journal of Harbin Institute of Technology, 31: 121-124).
    [16]
    洪嘉振, 蒋丽忠. 2000. 柔性多体系统刚-柔耦合动力学. 力学进展, 30: 15-20 (Hong J Z, Jiang L Z. 2000. Flexible multibody dynamics with coupled rigid and deformation motions. Advanced in Mechanics, 30: 15-20).
    [17]
    胡海昌. 1987. 多自由度结构固有振动理论. 北京: 科学出版社(Hu H C. 1987. Vibration Theory of Multi-degree-of-freedom Structure. Beijing: China Science Press).
    [18]
    胡起伟, 王广彦, 石全, 田霞. 2012. 爆炸冲击振动环境下电子装备损伤仿真研究. 兵工学报, 33: 13-18(Hu Q W, Wang G Y, Shi Q, Tian X. 2012. Research on electronic equipment damage simulation in explosion impact vibration environment. Acta Armamentarii, 33: 13-18).
    [19]
    黄春生, 吴杰, 范绪箕. 2004. 飞行器流场与结构温度场耦合数值分析. 力学与实践, 26: 24-26 (Huang C S, Wu J, Fan X J. 2004. Coupled numerical simulation of supersonic flow field and heated structure offlying vehicles. Mechanics and Engineering, 26: 24-26).
    [20]
    黄海, 谭春林, 裴晓强. 2007. 卫星总体参数多学科优化与建模探讨. 航天器工程, 16: 38-42 (Huang H, Tan C L, Pei X Q. 2007. Discussion on modeling and multidisciplinary design optimization for the satellite system parameters. Spacecraft Engineering, 16: 38-42).
    [21]
    黄文虎, 曹登庆, 韩增尧. 2012. 航天器动力学与控制的研究进展与展望. 力学进展, 42: 367-394 (Huang W H, Cao D Q, Han Z Y. 2012. Advances and trends in dynamics and control of spacecrafts. Advances in Mechanics, 42: 367-394).
    [22]
    黄彦文, 薛明德, 程乐锦, 张逸凡. 2005. 含开口薄壁杆的大型空间结构热诱发弯扭振动. 清华大学学报: 自然科学版, 45: 262-266 (Huang Y W, Xue M D, Cheng L J, Zhang Y F. 2005. Thermally induced vibrations of large space structures including thin-walled open beam sections. Journal of Tsinghua University (Science and Technology), 45: 262-266).
    [23]
    蒋国伟, 周徐斌, 申军烽, 顾亦磊, 杜冬, 孔祥森. 2011. 某卫星微振动建模与仿真. 航天器环境工程, 28: 36-40 (Jiang G W, Zhou X B, Shen J F, Gu Y L, Du D, Kong X S. 2011. Modeling and simulation of micro-vibration for a satellite. Spacecraft Environment Engineering, 28: 36-40).
    [24]
    蒋建平, 李东旭. 2009. 智能太阳翼有限元建模与振动控制研究, 7: 164-167 (Jiang J P, Li D X. 2009. Research on finite element modeling and vibration control for smart solar array. Journal of Dynamics and Control, 7: 164-167).
    [25]
    李东旭, 刘望, 蒋建平. 2011. 空间桁架结构采用黏弹性阻尼的振动控制技术. 噪声与振动控制, 8: 46-50 (Li D X, Liu W, Jiang J P. 2011. Passive vibration control of space truss structure with viscoelastic dampers.Noise and Vibation Control, 8: 46-50).
    [26]
    李恩奇, 盛秀成, 申志彬, 王江枫. 2012. 被动约束层阻尼梁动力学优化研究. 机械强度, 34: 176-182 (Li E Q, Sheng X C, Shen Z B, Wang J F. 2012. Optimization of dynamics for beam with passive constrained layer damping. Journal of Mechanical Strength, 34: 176-182).
    [27]
    李辉, 丁桦. 2008. 一种基于比例反馈控制原理的动载荷时域反演方法. 计算力学学报, 5: 602-609 (Li H, Ding H. 2008. A novel load identification method on vibration test. Chinese Journal of Computational Mechanics, 5: 602-609).
    [28]
    李伟鹏, 黄海, 边边. 2009. 精密跟瞄Hexapod 平台研制及其振动控制. 航空学报, 30: 259-264 (Li W P, Huang H, Bian B. 2009. Design and vibration control of precision pointing hexapod. Acta Aeronautica Et Astronautica Sinica, 30: 259-264).
    [29]
    李新明, 岳志勇, 张俊刚, 冯咬齐. 2008. 力限控制技术的试验研究. 强度与环境, 35: 8-9 (Li X M, Yue Z Y, Zhang J G, Feng Y Q. 2008. The study of force limited method based on test. Structure & Environment Engineering, 35: 8-9).
    [30]
    李正举, 马兴瑞, 韩增尧. 2011. 振动试验力限条件设计复杂二自由度方法研究. 宇航学报, 32: 1-6 (Li Z J, Ma X R, Han Z Y. 2011. Complex two-degree-of-freedom system method for force specification in force limited vibration test. Journal of Astronautics, 32: 1-6).
    [31]
    李志鑫, 李小清, 陈学东, 陈鹿民. 2008. 有限元分析中边界条件对模态影响的研究. 中国机械工程, 19: 1083-1086 (Li Z X, Li X Q, Chen X D, Chen L M. 2008. The study on boundary conditions to the 的力控振动平台集成设计研究effect of mode analysis in FEA. China Mechanical Engineering, 19: 1083-1086).
    [32]
    林来兴, 张新邦. 1997. 空间交会对接多自由度仿真器. 计算机仿真, 14: 12-15 (Lin L X, Zhang X B. 1997. New multiple-freedom simulator for rendezvous and docking. Computer Simulation, 14: 12-15).
    [33]
    刘闯, 冯咬齐, 岳志勇. 2009. 虚拟振动试验与真实试验相关性分析. 装备环境工程, 6: 1-15 (Liu C, Feng Y Q, Yue Z Y. 2009. Correlation analysis between virtual and real vibration test. Equipment Environmental Engineering, 6: 1-15).
    [34]
    刘闯, 向树红, 冯咬齐. 2009. 卫星虚拟振动试验系统研究. 航天器环境工程, 26: 248-253 (Liu C, Xiang S H, Feng Y Q. 2009. Research on virtual vibration test system for satellite. Spacecraft Environment Engineering, 26: 248-253).
    [35]
    刘源, 董立珉, 孔宪仁等. 2013. 飞行器虚拟振动试验平台构建. 光学精密工程, 21: 1258-1264 (Liu Y, Dong L M, Kong X R, et al. 2013. Construction of virtual vibration testing platform for spacecraft. Optics and Precision Engineering, 21: 1258-1264).
    [36]
    刘铸永. 2008. 刚{ 柔耦合系统动力学建模理论与仿真技术研究. 上海: 上海交通大学(Liu Z Y. Study on modeling theory and simulation technique for rigid-flexible coupling systems dynamics. Shanghai: Shanghai Jiao Tong University).
    [37]
    吕扬名. 2011. 基于永磁伸缩驱动机构的力控振动平台集成设计研究. 上海: 上海交通大学(Lü Y M. 2011. Research on the force limited vibration stage based on electro-magnetic and permanent magnet drive mechanism. Shanghai: Shanghai Jiao Tong University).
    [38]
    马传帅, 文桂林, 周景宇, 韩汪利, 戴意愿. 2011. 月球车沙地行驶动力学建模与仿真. 机械工程学报, 47: 97-103 (Ma C S, Wen G L, Zhou J Y, Han W L, Dai Y Y. 2011. Whole-vehicle dynamical model and simulation for lunar rover traveling on the loose soil. Journal of Mechanical Engineering, 47: 97-103).
    [39]
    马兴瑞, 韩增尧, 邹元杰, 丁继峰. 2012. 航天器力学环境分析与条件设计研究进展. 宇航学报, 33: 1-12 (Ma X R, Han Z Y, Zou Y J, Ding J F. 2012. Review and assessment of spacecraft mechanical environment analysis and specification determination. Journal of Astronautics, 33: 1-12).
    [40]
    马兴瑞, 王本利, 苟兴宇. 2001. 航天器动力学-若干问题进展与应用. 北京: 科学出版社(Ma X R, Wang B L, Gou X Y. 2001. Spacecraft Dynamics: Advances and Applications. Beijing: Beijing Science Press).
    [41]
    马兴瑞, 于登云, 韩增尧, 邹元杰. 2006. 星箭力学环境分析与试验技术研究. 宇航学报, 27: 323-331 (Ma X R, Yu D Y, Han Z Y, Zou Y J. 2006. Research evolution on the satellite-rocket mechanical environment analysis & test technology. Journal of Astronautics, 27: 323-331).
    [42]
    毛勇建, 李玉龙. 2007. 爆炸分离冲击环境的模拟试验技术进展. 导弹与航天运载技术, 290: 37-44 (Mao Y J, Li Y L. 2007. Advances in simulation techniques of pyroshock environments. Missiles and Space Vehicles, 290: 37-44).
    [43]
    孟中杰, 陈凯, 闫杰. 2008. 高超声速飞行器机体/发动机耦合建模与控制. 宇航学报, 29: 1509-1514 (Meng Z J, Chen K, Huang P F, Yan J. 2008. The coupling model and control between scramjet and airframe for hypersonic vehicle. Journal of Astronautics, 29: 1509-1514).
    [44]
    齐晓军, 张逸波, 孙祥, 满孝颖, 姜海坚. 2011. 卫星虚拟振动试验仿真效果研究. 航天器环境工程, 28: 344-348 (Qi X J, Zhang Y B, Sun X Y, Man X Y, Jiang H J. 2011. The satellite virtual vibration tests. Spacecraft Environment Engineering, 28: 344-348).
    [45]
    齐晓军. 2011. 航天器振动试验控制技术研究. 长沙: 国防科学技术大学(Qi X J. 2011. Research on spacecraft vibration test control technology. Changsha: National University of Defense Technology).
    [46]
    邱吉宝, 王建民. 2007. 航天器虚拟动态试验技术研究及展望. 航天器环境工程, 24: 1-14 (Qiu J B, Wang J M. 2007. A review on virtual dynamic test techniques for space vehicles. Spacecraft Environment Engineering, 24: 1-14).
    [47]
    沈凤霞. 2006. 振动试验力限控制力参数测量技术. 航天器环境工程, 23: 282-287 (Shen F X. 2006. The measurement of force parameters in vibration test with force limited method. Spacecraft Environment Engineering, 23: 282-287).
    [48]
    时军委, 徐峰, 胡雪平, 肖余之. 2011. 对接机构动力学仿真. 上海航天, 28: 17-22 (Shi J W, Xu F, Hu X P, Xiao Y Z. 2011. Docking mechanism dynamic simulation. Aerospace Shanghai, 28: 17-22).
    [49]
    史红霞. 2009. 基于修正广义正交域的动载荷识别研究. 哈尔滨: 哈尔滨工业大学(Shi H X. 2009. Dynamic load identification based on modified generalized orthogonal region. Harbin: Harbin Institute of Technology).
    [50]
    宋健. 2000. 在推力和阻力作用下的飞行器横向振动分析. 中国工程科学, 2: 66-72 (Song J. 2000. Lateral vibration analyses of flying vehicle under thrust and drag. Engineering Science, 2: 66-72).
    [51]
    宋琼, 范宣华, 胡勇. 2010. 基于MATLAB 和有限元的虚拟振动试验系统. 装备环境工程, 7: 9-12 (Song Q, Fan X H, Hu Y. 2010. Virtual vibration test system based on MATLAB and FEA. Equipment Environmental Engineering, 7: 9-12).
    [52]
    宋文治. 2006. NASA 在声振领域研究的新成果. 强度与环境, 33: 58-64 (Song W Z. 2006. New achieve-ments in the vibroacoustic field of the NASA. Structure & Environment Engineering, 33: 58-64).
    [53]
    谭天水. 2005. 在轨可展开天线网面的形状记忆合金热变形控制. [硕士论文]. 西安: 西安电子科技大学. (Tan T S. 2005. Shape memory alloy control thermal deformation of the deployable antenna mesh at orbit. [Master Thesis]. Xi'an: Xidian University).
    [54]
    谭雪峰, 阎绍泽. 2010. 星箭包带式连接结构动力学研究进展. 导弹与航天运载技术, 1: 1-6 (Tan X F, Yan S Z. 2010. Evolution of research on dynamics of clamp band system between satellite and launch vehicle. Missiles and Space Vehicles, 1: 1-6).
    [55]
    唐照千, 黄文虎. 1990. 振动与冲击手册. 第2, 3 卷. 北京: 国防工业出版社(Tang Z Q, Huang W H. 1990. Vibration and Shock Handbook, Volumes 2 and 3. Beijing: National Defense Industry Press).
    [56]
    陶建忠, 雷勇军. 2003. 大型柔性太阳电池翼模态参数计算. 湖南理工学院学报(自然科学版), 16: 33-36 (Tao J Z, Lei Y J. 2003. Modal characteristics analysis of large flexible solar panel. Journal of Hunan Institute of Science and Technology (Natural Science Edition), 16: 33-36).
    [57]
    田强, 张云清, 陈立平, 覃刚. 2010. 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, 40: 189-202 (Tian Q, Zhang Y Q, Chen L P, Qin G. 2010. Advances in the absolute nodal coordinate method for the flexible multibody dynamics. Advances in Mechanics, 40: 189-202).
    [58]
    王大鹏. 2010. 有效载荷机柜结构优化设计. 航天器工程, 19: 34-39 (Wang D P. 2010. Optimization for payload rack structure design. Spacecraft Engineering, 19: 34-39).
    [59]
    王飞, 陈卫东. 2010. 爆炸冲击载荷作用下板壳结构数值仿真分析. 强度与振动, 37: 36-39 (Wang F, Chen W D. 2010. The numerical simulation analysis of the shell structure subjected to contact explosion. Structure & Environment Engineering, 37: 36-39).
    [60]
    王静, 陈海波, 王靖. 2013. 基于精细积分的冲击载荷时域识别方法研究. 振动与冲击, 32: 81-85 (Wang J, Chen H B,Wang J. 2013. Impulsive load identification in time domain based on precise time integration method. Journal of Vibration and Shock, 32: 81-85).
    [61]
    王军评, 毛勇建, 黄含军. 2013. 点式火工分离装置冲击载荷作用机制的数值模拟研究. 振动与冲击, 32: 9-14 (Wang J P, Mao Y J. 2013. Numerical simulation for impulsively loading mechanism of a point pyrotechnic separation device. Journal of Vibration and Shock, 32: 9-14).
    [62]
    王珂晟, 雷勇军, 朱晓莹. 2004. 系统级产品振动试验的探讨与研究. 振动与冲击, 23: 112-115 (Wang K S, Lei Y J, Zhu X Y. 2004. Investigation on vibration testing for system level equipments. Journal of Vibration and Shock, 23: 112-115).
    [63]
    王尚文. 1986. 飞行器结构动力学. 西安: 西北工业大学出版社(Wang S W. 1986. Structural Dynamics of Aircraft. Xi'an: Northwestern Polytechnical University Press).
    [64]
    王晓耕. 2002. 力限技术的发展和应用前景. 航天器环境工程, 19: 23-26 (Wang X G. 2002. Development and application prospects of force limited technique. Spacecraft Environment Engineering, 19: 23-26).
    [65]
    王兴贵, 韩松臣, 荣丽, 赵阳. 1999. 周边式对接机构的航天器首次接触撞击点的确定. 宇航学报, 20: 49-57 (Wang X G, Han S C, Rong L, Zhao Y. 1999. Determining the position of the first contact points for the space vehicles with androgynous peripheral docking mechanism. Journal of Astronautics, 20: 49-57).
    [66]
    吴艳红, 王晓晖, 马斌捷, 荣克林, 李双. 2007. 爆炸螺栓盒的爆炸模拟与冲击强度计算. 强度与环境, 34: 10-15 (Wu Y H, Wang X H, Ma B J, Rong K L, Li S. 2007. The simulation of explosion and the calculation of the impact strength of the explosive bolt box. Structure & Environment Engineering, 34: 10-15).
    [67]
    夏利娟, 郑靖明, 金咸定. 2002. 工程结构的优化设计方法与应用. 上海交通大学学报, 36: 1573-1575 (Xia L J, Zheng J M, Jin X D. 2002. Optimal design of engineering structures and its application. Journal of Shanghai Jiao Tong University, 36: 1573-1575).
    [68]
    熊旭, 尚海滨, 王帅. 2013. 小行星采样返回探测任务发射机会搜索//中国宇航学会深空探测技术专业委员会第十届学术年会论文集(Xiong X, Shang H B, Wang S. 2013. Opportunity options for rendezvous, flyby and sample return mission to different spectral-type asteroids//The 10th Seminar of Deep Space Exploration Department of China Society of Astronautics).
    [69]
    徐福祥. 2002. 卫星工程. 北京: 中国宇航出版社(Xu F X. 2002. Satellite Engineering. Beijing: China Astronautic Publishing House).
    [70]
    徐梅. 2010. 复杂结构分布载荷识别的动态标定技术研究. 南京: 南京航空航天大学(Xu M. 2010. The dynamic calibration distribute load identification on complex structures. Nanjing: Nanjing University of Aeronautics and Astronautics).
    [71]
    杨炳渊, 宋伟力. 1995. 用当地流活塞理论计算大攻角翼面超声速颤振. 振动与冲击, 15: 60-63 (Yang B Y, Song W L. 1995. Analysis of supersonic-hypersonic flutter of lifting surfaces base on piston theory. Journal of Vibration and Shock, 15: 60-63).
    [72]
    杨国华, 战兴群. 2006. 空间对接综合试验台大回路系统控制模式的研究. 液压与气动, 5: 41-43 (Yang G H, Zhan X Q. 2006. Study on control model of big-loop system about Stewart flat of space docking general test stand. Chinese Hydraulics & Pneumatics, 5: 41-43).
    [73]
    杨庆俊, 王晓雷. 2006. 主被动一体化八作动器隔振平台研究//第四届全国流体传动与控制学术会议论文集. (Yang Q J, Wang X L. 2006. Integrated active and passive vibration isolation using pneumatic octo-strut platform//The 4th FPTC).
    [74]
    姚德源, 王其政. 1995. 统计能量分析原理及其应用. 北京: 北京理工大学出版社(Yao D Y, Wang Q Z. 1995. Statistical Energy Analysis Theory and Application. Beijing: Beijing Institute of Technology Press).
    [75]
    殷学刚, 陈淮, 塞开林. 1991. 结构振动分析的子结构方法. 北京: 中国铁道出版社(Yin X G, Chen H, Sai K L. 1991. Substructure Method of Structure Dynamics. Beijing: China Railway Publishing House).
    [76]
    尹立中, 邹经湘, 王本利. 2000. 俯仰运动圆柱贮箱中液体的非线性晃动. 力学学报, 32: 280-290 (Yin L Z, Zou J X, Wang B L. 2000. Nonlinear sloshing of liquid in a circle cylindrical container under pitching excitation. Acta Mechanica Sinica (in Chinese), 32: 280-290).
    [77]
    虞自飞, 周徐斌, 申军烽. 2013. 卫星飞轮隔振与吸振联合减振系统设计//中国空间科学学会2013 年空间光学与机电技术研讨会会议论文集, 西安, 241-246 (Yu Z F, Zhou X B, Shen J F. 2013. Design on the joint vibration reduction of isolation and dynamic vibration absorber for flywheel//Seminar of Chinese Society of Space Research, 241-246).
    [78]
    袁家军, 陈珅艳, 黄海. 2006. 基于Patran/Nastran 的结构优化系统的工程应用. 北京航空航天大学学报, 32: 125-129 (Yuan J J, Chen K Y, Huang H. 2006. Engineering applications of structural optimization system based on Patran/Nastran. Journal of Beijing University of Aeronautics and Astronautics, 32: 125-129).
    [79]
    岳志勇, 张俊刚, 冯咬齐. 2006. 力限控制方法试验验证技术研究. 航天器环境工程, 23: 227-231 (Yue Z Y, Zhang J G, Feng Y Q. 2006. The application of force limited method in vibration test. Spacecraft Environment Engineering, 23: 227-231).
    [80]
    岳志勇, 张俊刚, 冯咬齐. 2007. 力限试验夹具及FMD 技术研究. 航天器环境工程, 24: 244-247 (Yue Z Y, Zhang J G, Feng Y Q. 2007. The study of fixture and FMD in force limited vibration tests. Spacecraft Environment Engineering, 24: 244-247).
    [81]
    张博文, 王小勇, 胡永力. 2012. 微振动对高分辨率空间相机成像影响的集成分析. 航天返回与遥感, 33: 60-66 (Zhang B W, Wang X Y, Hu Y L. 2012. Integrated analysis on effect of micro-vibration on high resolution space camera imaging. Spacecraft Recovery and Remote Sensing, 33: 60-66).
    [82]
    张崇峰. 1999. 空间对接六自由度半物理仿真的研究. 航天控制, 1: 70-74 (Zhang C F. 1999. Study on six-degree-of-freedom simulation for docking. Aerospace Control, 1: 70-74).
    [83]
    张建华. 2005. 航天产品的爆炸冲击环境技术综述. 导弹与航天运载技术, 276: 30-36 (Zhang J H. 2005. Pyroshock environment of missiles and launch vehicles. Missiles and Space Vehicles, 276: 30-36).
    [84]
    张俊刚, 庞贺伟. 2005. 振动试验中的力限控制技术. 航天器环境工程, 22: 253-256 (Zhang J G, Pang H W. 2005. The force limited control technique in vibration test. Spacecraft Environment Engineering, 22: 253-256).
    [85]
    张俊刚, 岳志勇, 李新明. 2008. 力限控制技术应用研究. 航天器环境工程, 25: 346-347 (Zhang J G, Yue Z Y, Li X M. 2008. The application of force limited method. Spacecraft Environment Engineering, 25: 346-347).
    [86]
    张少雄, 王利永, 孔泉. 2006. 网格粗细对于有限元模态分析计算的影响. 武汉理工大学学报, 28: 92-94 (Zhang S X, Wang L Y, Kong Q. 2006. On the influence of mesh size upon the FE modal analysis of structures. Journal of Wuhan University of Technology, 28: 92-94).
    [87]
    张小达, 夏益霖. 2002. 爆炸分离冲击试验方法标准研究. 航天标准化, 6: 1-5 (Zhang X D, Xia Y L. 2002. Research on the pyroshock test standard. Aerospace Standardigation, 6: 1-5).
    [88]
    张逸波, 齐晓军, 张丽新, 付国庆. 2009. 卫星三向力限FMD 振动夹具设计. 航天器环境工程, 26: 358-365 (Zhang Y B, Qi X J, Zhang L X, Fu G Q. 2009. Design of the vibration fixture for satellite three-directional FMD. Spacecraft Environment Engineering, 26: 358-365).
    [89]
    张永涛, 周徐斌, 杜冬等. 2015. 一种星箭动态界面力识别方法. 航天器工程, 24: 62-69 (Zhang Y T, Zhou X B, Du D, et al. 2015. An identification methok for satellite-launcher dynamic interface force. Spacecraft Engineering, 24: 62-69).
    [90]
    张运良, 林皋, 王学永等. 2004. 一种改进的动态载荷时域识别方法. 计算力学学报, 21: 209-215 (Zhang Y L, Lin G, Wang X Y, et al. 2004. An improved method of dynamic load identification in time domain. Chinese Journal of Computational Mechanics, 21: 209-215).
    [91]
    张振华, 杨雷, 庞世伟. 2009. 高精度航天器微振动力学环境分析. 航天器环境工程, 26: 528-534 (Zhang Z H, Yang L, Pang S W. 2009. Jitter environment analysis for micro-precision spacecraft. Spacecraft Environment Engineering, 26: 528-534).
    [92]
    张正平, 王宇宏, 朱曦全. 2006. 动力学综合环境试验技术现状和发展. 装备环境工程, 3: 7-11 (Zhang Z P, Wang Y H, Zhu X Q. 2006. Current state and developing trend of combined dynamic environmental test. Equipment Environmental Engineering, 3: 7-11).
    [93]
    赵慧, 张尚盈. 2007. Stewart 平台雅克比矩阵分析. 重庆科技学院学报, 9: 142-144 (Zhao H, Zhang S Y. 2007. On Jacobian matrix of Stewart platform. Journal of Chongqing University of Science and Technology, 9: 142-144).
    [94]
    赵慧, 张尚盈. 2008. 空间对接整体动力学仿真系统稳定性分析. 武汉科技大学学报(自然科学版), 31: 87-90 (Zhao H, Zhang S Y. 2008. Stability analysis of the whole dynamics simulation system of space docking. Journal of Wuhan University of Science and Technology (Natural Science Edition), 31: 87-90).
    [95]
    赵阳, 曹喜滨, 王兴贵, 邵成勋. 1999. 空间对接机构差动式缓冲阻尼及传动系统力学特性研究. 空间科学学报, 19: l73-l80 (Zhao Y, Cao X B, Wang X G, Shao C X. 1999. Dynamic characteristics on differential cushion damping and transmission system of space docking mechanism. Chinese Journal of Space Science, 19: l73-l80).
    [96]
    郑开陛. 1984. 模拟火工品冲击的新方法. 强度与环境, 12: 10-19. (Zheng K B. 1984. New technique to simulation pyrotechnic shock. Structure & Environment Engineering, 12: 10-19).
    [97]
    周成, 李家文, 李永等. 2013. 多维虚拟振动试验系统设计及应用. 火箭推进, 39: 85-91 (Zhou C, Li J W, L Y, et al. 2013. Design and application of multi-dimensional virtual vibration testing system. Journal of Rocket and Propulsion, 39: 85-91).
    [98]
    周莹, 宋汉文. 2008. 力控振动试验与过试验现象分析. 振动与冲击, 24: 82-84 (Zhou Y, Song H W. 2008. Analysis of a vibration overtest problem and a force limited control vibration test. Journal of Vibration and Shock, 24: 82-84).
    [99]
    邹猛, 李建桥, 李因武等. 2007. 刚性轮—月壤相互作用预测模型及试验研究//中国农业工程学会学术年会, 23: 119-123 (Zou M, Li J Q, Li Y W, et al. 2007. Predicton model and experimental study on the interaction of ridgid-wheel and lunar soil//Senimar of Chinese Society of Agricultural Engineering, 23: 119-123).
    [100]
    Abramson H. N. 1966. The dynamic behaviour of liquids in moving containers. NASA SP-106.
    [101]
    Akyild{z H, Unal N E. 2006. Sloshing in a three-dimensional rectangular tank: numerical simulation and experimental validation. Ocean Engineering, 33: 2135-2149.
    [102]
    Aliabadi S, Johnson A, Abedi J. 2003. Comparison of finite element and pendulum models for simulation of sloshing. Computers & Fluids, 32: 535-545.
    [103]
    Andre C, Ramin S, Yvan S. 2004. Force-limited vibration complex two-degree-of-freedom system method. AIAA Journal, 42: 1208-1217.
    [104]
    Appolloni M, Cozzani A. 2005. Use of advanced integrated CAE tools to provide an end-to-end simula-tion of payload testing on Hydra//Proceedings of Seminar on Integrated open CAD/CAE platforms for Mechanical Engineering, Noordwijk: 579-591.
    [105]
    Arthur E P V. 2006. The simulation of violent free-surface dynamics at sea and in space//Proceedings of European Conference on Computational Fluid Dynamics, TU Delft, Netherland.
    [106]
    Banerjee A K, Kane T R. 1989. Dynamics of a plate in large overall motion. Journal of Applied Mechanics, 56: 887-892.
    [107]
    Beal T R. 1965. Dynamic stability of a flexible missile under constant and pulsating thrust. Journal of Aircraft, 3: 486-494.
    [108]
    Beranek L L, Ver I L. 1992. Noise and Vibration Control Engineering-principles and Applications. John Wiley & Sons, Inc.
    [109]
    Bertin J J. 1994. Hypersonic aero-thermo dynamics. American Institute of Aeronautics and Astronautics, Washington DC. PP. 240.
    [110]
    Betts E J, Vansant K, Paulson C, et al. 2008. Smart testing using virtual vibration testing//Proceeding of the 24th Aerospace Testing Seminar (ATS)., Manhattan Beach: 103-111.
    [111]
    Bialke B. 1997. A compilation of reaction wheel induced spacecraft disturbances//Proceeding s of the 20th Annual American Astronautically Society Guidance and Control Conference.
    [112]
    Blake R E. 1956. The need to control the output impedance of vibration and shock machines shock and vibration bulletin. Shock and Vibration Bulletin, 23: 59-64.
    [113]
    Boley B A. 1956. Thermally induced vibrations of beams. Journal of the Aeronautical Sciences, 23: 179-181.
    [114]
    Book W J. 1984. Recursive Lagrangian dynamics of flexible manipulator arms. The International Journal of Robotics Research, 3: 87-100.
    [115]
    Brauckmann G J. 1998. X-34 vehicle aerodynamic characteristics. NASA Langley Research Center, Hamp-ton, VA 23681-0001.
    [116]
    Cambier F, Conti C, Dehombreux P. 1998. Development of a test facility to simulate pyroshock environments in a laboratory//Proceedings of the 5th International Conference on Structures Under Shock and Impact: 273-282.
    [117]
    Candler G V. 1998. High enthalpy flow simulation challenges. AIAA Paper 98-2749.
    [118]
    Chang K Y. 2002. Structural loads prediction in force-limited vibration testing. Jet Propulsion Laboratory, California Institute of Technology, Spacecraft & Launch Vehicle Dynamic Environmental Workshop, 25-27.
    [119]
    Charles R, McClinton, Vincent L, Rausch, et al. 2005. Preliminary X-43 flight test results. Acta Astronau-tica, 57: 266-276.
    [120]
    Chen H J, Bishop Jr R M, Agrawal B N. 2003. Payload pointing and active vibration isolation using hexapod platforms//44th AIAA/SAME/ASCE/AHS structures and structural dynamics and materials conference: 30-36.
    [121]
    Chen Y G, Djidjeli K, Price W G. 2009. Numerical simulation of liquid sloshing phenomena in partially filled containers. Computers & Fluids, 38: 830-842.
    [122]
    Chen Y K, Henline W D, Tauber M E. 1995. Mars pathfinder trajectory based heating and ablation calculations. Journal of Spacecraft and Rockets, 32: 225-230.
    [123]
    Ciskowski R D, Brebbia C A. 1991. A Boundary Element Methods in Acoustics. Southampton: Computa-tional Mechanical Publications.
    [124]
    Cotoni V, Shorter P J, Langley R S. 2007. Numerical and experimental validation of a hybrid finite element-statistical energy analysis method. Journal of the Acoustical Society of America, 122: 259-270.
    [125]
    Cui E J. 2003. Modern mechanics and aero-astronautics. distinguished lecture on fluid mechanics. 2002-2003 Annual Meeting, HKSTAM, Hong Kong.
    [126]
    Culler A J, 2010. Coupled fluid-thermal-structural modeling and analysis of hypersonic flight vehicle struc-tures. The Ohio State University.
    [127]
    Deborah A, David P. 2006. Force limited vibration test of HESSI imager. IIAV's ICSV7.
    [128]
    Desanghere G, Snoeys R. 1985. Indirect identification of excitation forces by modal coordinate transforma-tion//Proceedings of the 3rd IM AC, 685-690.
    [129]
    Ding L, Gao H B, Deng Z Q. 2009. Slip ratio for lugged wheel of planetary rover in deformable soil: definition and estimation//The IEEE/RSJ International Conference on Intelligent Robots and System, St. Louis, USA: 3343-3348.
    [130]
    Drisch H P. 1970. Thermally induced vibrations of long thin-walled cylinders of open section. Journal of Spacecraft and Rockets, 7: 897-905.
    [131]
    Eswaran M, Saha U K, Maity D. 2009. effect of ba²es on a partially filled cubic tank: numerical simulation and experimental validation. Computers & Structures, 87: 198-205.
    [132]
    Eyerman C E, Shea J F. 1990. A systems engineering approach to disturbance minimization for spacecraft utilizing controlled structures technology. MIT SERC Report: 2-90.
    [133]
    Ferrara V, Culla A, Preve A. 2007. High frequency vibroacoustic analyses on VEGA launch vehicle//28th AIAA Aeroacoustics Conference.
    [134]
    Foster C L, Nker M L, Nurre G S. 1995. Solar-array-induced disturbance of the Hubble space telescope pointing system, Journal of Spacecraft and Rockets, 32: 634-644.
    [135]
    Friedmann P P. 2003. Hypersonic aeroelasticity and aerothermoelasticity with application to reusable launch vehicles. AIAA-2003-7014.
    [136]
    Giaime J, Saha P, Shoemaker D. 1996. A passive vibration isolation stack for LIGO: design, modeling, and testing. Review of Scientific Instruments, 67: 208-214.
    [137]
    Gibson G R, Janssen S G, Bradford L F, Groom R S. 2004. Overview of the development of dynamic environments for atlas v launch vehicles. Journal of Spacecraft and Rockets, 41: 779-786.
    [138]
    Gladwell G M L. 1964. Branch mode analysis of vibrating systems. Journal of Sound and Vibration, 1: 41-59.
    [139]
    Gou X Y, Ma X R, Wang B L, et al. 2001. Synchronous Hopf bifurcation and damping osmosis phenomena of a liquid-spacecraft nonlinear coupling system. AIAA Journal, 39: 225-232.
    [140]
    Hambleton J P, Drescher A. 2008. Modeling wheel-induced rutting in soils: Indentation. Journal of Ter-ramechanics, 45: 201-211.
    [141]
    Hambleton J P, Drescher A. 2009. Modeling wheel-induced rutting in soils: Rolling. Journal of Terrame-chanics, 46: 35-47.
    [142]
    Hansen M, Starkey J M. 1990. On predicting and fin-proving the condition of modal-model-based indirect force measurement algorithms//Proceedings of the 8th IMAC, Kissimcc FL, USA: 115-120.
    [143]
    Huang Q T, Zhang S Y, Han J W. 2004. A hardware-in-the-loop spacecraft docking simulation system and its stability analysis//Proceeding of the Sixth International Conference on Fluid Power Transmission and Control, Hangzhou, China, 101-106
    [144]
    Hughes W, McNelis A, Himelblau H. 1999. Investigation of acoustic fields for the cassini spacecraft: rever-berant versus launch environments. NASA/TM, 209387: 1-21.
    [145]
    Hughes W, McNelis A. 1997a. Acoustic testing of the cassini spacecraft and titan IV payload fairing. I. Introduction and test configuration. NASA Technical Memorandum, 107474: 1-10.
    [146]
    Hughes W, McNelis A. 1997b. Acoustic testing of the cassini spacecraft and titan IV payload fairing. II. Results. NASA Technical Memorandum, 107475: 1-8.
    [147]
    Hunter N, Lake J. 1996. Force controlled vibration tests using voltage current measurements//Proceedings-Institute of Environmental Sciences.
    [148]
    Hurty W C. 1960. Vibrations of structural systems by component mode synthesis. Journal of the Engineer-ing Mechanics Division, ASCE, 86: 51-70.
    [149]
    Iannotta B. 2000. Slosh, rattle and roll. New Scientist, 27: 32-35.
    [150]
    Ibrahim R A. 2008. Recent advances in nonlinear passive vibration isolators. Journal of Sound and Vibra-tion, 314: 371-452.
    [151]
    John O C, Fabio P. 1994. Force estimation using operational data//Proceedings of 8nd International Modal Analysis Conference, 1586-1592.
    [152]
    Johnston J D, Thornton E A. 1999. Thermal snap of satellite solar panels//Proceedings of the 1999 Flight Mechanics Symposium, NASA CP 209235, 215-229.
    [153]
    Kane T R, Ryan R R, Baneijee A K. 1987. Dynamics of a cantilever beam attached to a moving base. Journal of Guidance, Control and Dynamics, 10: 139-151.
    [154]
    Karlsson S E S. 1996. Identification of external structural loads from measured harmonic responses. Journal of Sound and Vibration, 196: 59-74.
    [155]
    Kienke S E, Lauffer J P, Gregory D L, et al. 1996. The Vibration Virtual Environment for Test Optimization. New Mexico: S. V. Symp, 67-76.
    [156]
    Kienke S E, Reese G M, Schoof L A, et al. 1996. Model test optimization using VETO (Virtual Environment for Test Optimization). Sandia Report SAND, 95-2591: 1-7.
    [157]
    Kilenke S, Baca T. 1996. Structural dynamics test simulation and optimization for aerospace compo-nents//Proceedings of the Second Test and Evaluation International Aerospace Forum,Washington: 82-89
    [158]
    Kolaini A R, Kissil A, Childs B W. 2009. Vibro-acoustic analysis of lightweight structures//The 2009 S/C & L/V Dynamic Environment Workshop, El Segundo, USA.
    [159]
    Lalanne C. 2002. Mechanical vibration and shock, volume II: Mechanical shock. Hermes Penton Ltd., New York
    [160]
    Lane S, Kennedy S, Richard R. 2007. Noise transmission studies of an advanced grid-stiffened composite fairing. Journal of Spacecraft and Rockets, 44: l131-1139.
    [161]
    Lav R K, Salokhe V M, Jayasuriya H P W. 1998. Experimental validation of distinct element simulation for dynamic wheel-soil interaction. Journal of Terramechanics, 35: 119-135.
    [162]
    Lawrence J O. 1965. Aerothermoelasticity: its impact on stability and control of winged aerospace vehicles. Journal of Aircraft, 2: 517-526.
    [163]
    Lee J D, Wang B L. 1988a. Optimal control of a flexible robot arm. Computers & Structures, 29: 459-467.
    [164]
    Lee J D, Wang B L. 1988b. Dynamic equations for a two-Link flexible robot arm. Computers & Structures, 29: 467-477.
    [165]
    Li H Y, Dong W Z, Zhu G L. 2006. Numerical simulation of non-equilibrium viscous flows in hypersonic nozzles. Acta Aeronautica Et Astronautica Sinica, 27: 204-207.
    [166]
    Li Y C. 2003. Robust control of a two-link manipulator with neural network based quasi-static deflection compensation//The American Control Conference, Changchun, China, 5258-5263.
    [167]
    Lieberman P. 1982. Pyrotechnic simulation techniques//Proceedings of the 7th Aerospace Testing Seminar.
    [168]
    Lighthill M. J. 1953. Oscillating airfoils at high mach numbers. Journal of the Aeronautical Sciences, 20: 402-406.
    [169]
    Lillie C F, Bronowicki A J. 2004. Adaptation in space telescopes//The 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conf., Palm Springs, CA, AIAA, 2064: 2007.
    [170]
    Luppes R, Helder J A, Veldman A E P. 2006. The numerical simulation of liquid sloshing in micrograv-ity//Proceedings of European Conference on Computational Fluid Dynamics, TU Delft, Netherland.
    [171]
    Mercier R, McClinton C. 2003. Hypersonic propulsion-transforming the future of flight. AIAA Paper 2003-2732.
    [172]
    Morrow C T. 1960. Application of mechanical impedance concept to shock and vibration testing. Los Angeles, CA, TRW Report AD-608030.
    [173]
    Murfin, W B. 1968. Dual specification in vibration testing. Shock and Vibration Bulletin, 38: 109-113.
    [174]
    Ory H, Glaser H, Holzdepp D. 1985. The reconstruction of forcing function based on aero elasticity and structural dynamics. Aschen, FRG, USA: 164-168.
    [175]
    Ory H, Glaser H, Holzdeppe D. 1986. Quality of modal analysis and reconstruction of forcing function based on measured output data//Proceeding of 4th IMAC, USA: 350-357.
    [176]
    Patil M J, Hodges D H, Cesnik C E S. 2000. Nonlinear aeroelastic analysis of complete aircraft in subsonic flow. Journal of Aircraft, 37: 753-760.
    [177]
    Ramin S, Nicolas E. 2003. E±cient estimation of effective mass for complex structures under base excitations. 49: 135-143.
    [178]
    Ricci S, Peetrs B, Debille J, et al. 2008. Virtual shaker testing: A novel approach for improving vibration test performation//International Conference on Noise and Vibration Engineering, Leuven: Katholieke University Leuven: 1767-1782.
    [179]
    Ricci S, Peetrs B. 2009. Virtual shaker testing for predicting and improving vibration test performa-tion//Proceedings of the IMAC-VII, Orlando, 1-16.
    [180]
    Sabelhaus P, Decker J. 2004. An overview of the JamesWebb Space Telescope (JWST) project//Proceedings of SPIE Vol. 5487 (SPIE, Bellingham, WA, 2004).
    [181]
    Sagnier P. Marraffa L. 1989. Parametric study of thermal and chemical non-equilibrium nozzle flow. AIAA Paper 89-1858.
    [182]
    Saltzman E J. 1999. Flight-determined subsonic lift and drag characteristics of seven lifting-body and wing-body reentry vehicle configurations with truncated bases//Analytical Services & Materials Edwards, California.
    [183]
    Scharton T D, Chang K. 1997. Force limited vibration testing of Cassini spacecraft and instruments//Los Angeles, CA: IES 17th Aerospace Testing Seminar.
    [184]
    Scharton T D, Kern D L. 1988. Using the VAPEPS program to support the TOPEX spacecraft design effort//Proceedings of the 59th Shock and Vibration Sym-posium, 21-36.
    [185]
    Scharton T D. 1993. Force limited vibration testing at JPL//Proceedings of the Institute of Environmental Sciences 14th Aerospace Testing Seminar: 241-251.
    [186]
    Scharton T D. 1995. Vibration-test force limits derived from frequency-shift method. AIAA, Journal of Spacecraft and Rockets, 32: 312-316.
    [187]
    Scharton T D. 1997. Force Limited Vibration Testing Monograph. NASA Reference Publication RP: 1403.
    [188]
    Scharton T D. 1997. Force-limited vibration testing monograph. NASA RP: 1403.
    [189]
    Scharton T D. 2003. Force limited vibration testing, NASA technical handbook. NASA-HDBK-7004B, Jan.
    [190]
    Schmidt D, Velapoldi J. 1999. Flight dynamics and feedback guidance issues for hypersonic air-breathing vehicles//Proceedings of the 1999 Guidance, Navigation, and Conlrol Conference, Portland.
    [191]
    Scott C D. 1992. Wall catalytic recombination and boundary conditions in nonequilibrium hypersonic flows with applications. Advances in Hypersonics: Modeling Hypersonic Flows, 2: 177-249.
    [192]
    Seungmook C. 2004. effect of follower forces on aeroelastic stability of flexible structures. [PHD. Thesis], Georgia Institure of Technology, GA.
    [193]
    Shorter P J, Langley R S. 2005. Vibro-acoustic analysis of complex systems. Journal of Sound and Vibration, 288: 669-699.
    [194]
    Slater J P. 1964. Taming the general-purpose vibration test. Shock and Vibration Bulletin, 33: 211-217.
    [195]
    Souto-Iglesias A, Delorme L, Perez-Rojas L, Abril-Perez S. 2006. Liquid moment amplitude assessment in sloshing type problems with smooth particle hydrodynamics. Ocean Engineering, 33: 1462-1484.
    [196]
    Starkey J M, Merrill G L. 1989. On the 1ll-conditioned nature of indirect force measurement techniques. International Journal of Analytic and Experimental Modal Analysis, 4: 103-108.
    [197]
    Sunada W, Dubowsky S. 1971. The application of finite element methods to the dynamic analysis of flexible spatial and co-planar linkage systems. Journal of Mechanical Design, 103: 643-651.
    [198]
    Tanaka K, Sugeno M. 1992. Stability analysis and design of fuzzy control systems. Fuzzy Sets and Systems, 45: 135-156.
    [199]
    Thayer D, Campbell M, Vagners J. 2002. Six-axis vibration isolation system using soft actuators and multiple sensors. Journal of Spacecraft and Rockets, 39: 206-212.
    [200]
    Thornton E A, Dechaumphai P. 1987. Finite element prediction of aerothermal-structural interaction of aerodynamically heated panels. AIAA Paper, 87-1610.
    [201]
    Thornton E A, Foster R S. 1992. Dynamic response of rapidly heated space structures. AIAA, Washington, D. C., 451-477.
    [202]
    Thornton E A, Kim Y A. 1993. Thermal induced bending vibrations of a flexible rolled-up solar array. Journal of Spacecraft and Rockets, 30: 438-448.
    [203]
    Thornton E A, Paul D B. 1985. Thermal-structural analysis of large space structures: an assessment of recent advances. Journal of Spacecraft and Rockets, 22: 385-393.
    [204]
    Turcic D A, Midha A. 1984. Dynamic analysis of elastic mechanism systems, Part I: Applications. Journal of Dynamic Systems, Measurements and Control, 106: 243-248.
    [205]
    Uebelhart S A. 2001. Conditioning, reduction, and disturbance analysis of large order integrated models for space-based telescopes. Massachusetts Institute of Technology.
    [206]
    Veldman A, Gerrits J, Luppes R, Helder J, Vreeburg J. 2007. The numerical simulation of liquid sloshing on board spacecraft. Journal of Computational Physics, 224: 82-99.
    [207]
    Weilmuenster K J, Gnoffo P A, Greene F A. 1993. Navier-Stokes simulations of the shuttle orbiter aerody-namic characteristics with emphasis on pitch trim and body flap. AIAA Paper 93-2814.
    [208]
    Wijker J. 2008. Spacecraft Structures. New York: Springer Publishing Company.
    [209]
    Wu J J. 1976. Missile stability using finite elements: an unconstrained variational approach. AIAA Journal, 14: 313-319.
    [210]
    Yang R C, Saffell H R. 1972. Development of a waveform synthesis technique: a supplement to response spectrum as a definition of shock environment. Journal of Sound and Vibration, 42: 45-53.
    [211]
    Yarza A, Castro O, Santiago-Prowald J. 2010. Reflector vibroacoustic response to launch acoustic excita-tion//European Conference on Antennas and Propagation 2010, Barcelona.
    [212]
    Zhang D G, Zhou S F. 2006. Dynamics analysis of flexible-link and flexible-joint robots. Applied Mathematics and Mechanics, 27: 695-704.
    [213]
    Zhang Y T, Zhou X B, Zhang J, et al. A novel identifying strategy for MDOF dynamic interface force based on strain monitoring//The 14th ISCOPS, Xi'an.
    [214]
    Zimpfer D, Spehar P. 1996. STS-71shuttle/mir GNC mission overview. American Astronautical Society, Sandi ego, CA: 441-460.
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