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 |
[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.
|