| [1] | 陈士橹, 祝小平, 唐硕 等. 挠性航天器动力学的几个研究方向. 世界科技研究与发展, 1998,20(6):43-47 | | [1] | ( Chen Shilu, Zhu Xiaoping, Tang Shuo, et al. Some research fields in astrodynamics of flexible spacecraft. World Sci-Tech R & D, 1998,20(6):43-47 (in Chinese)) | | [2] | 曲广吉. 航天器动力学工程. 北京: 中国科学技术出版社, 2000 | | [2] | ( Qu Guangji. Spacecraft Dynamics Engineering Beijing: Science and Technology of China Press, 2000 (in Chinese)) | | [3] | Wang Y, Huston R. A lumped parameter method in the nonlinear analysis of flexible multibody systems. Computers & Structures, 1994,50(3):421-432 | | [4] | Sun C, He W, Hong J. Neural network control of a flexible robotic manipulator using the lumped spring-mass model// IEEE Transactions on Systems, Man, and Cybernetics: Systems, 2016 | | [5] | Benson D, Hallquist J. A simple rigid body algorithm for structural dynamics programs. International Journal for Numerical Methods in Engineering, 1986,22(3):723-749 | | [6] | Belytschko T, Hsieh B. Non-linear transient finite element analysis with convected co-ordinates. International Journal for Numerical Methods in Engineering, 1973,7(3):255-271 | | [7] | 蔡国平, 洪嘉振. 旋转运动柔性梁的假设模态方法研究. 力学学报, 2005,37(1):48-56 | | [7] | ( Cai Guoping, Hong Jiazhen. Research on hypothetical modal method of flexible beam with rotating motion. Chinese Journal of Theoretical and Applied Mechanics, 2005,37(1):48-56 (in Chinese)) | | [8] | Shabana AA. Flexible multibody dynamics: Review of past and recent developments. Multibody System Dynamics, 1997,1(2):189-222 | | [9] | 周志成, 王兴龙, 曲广吉. 大型空间柔性组合航天器动力学建模与控制. 中国科学: 物理学力学天文学, 2019,42(2):62-73 | | [9] | ( Zhou Zhicheng, Wang Xinglong, Qu Guangji. Dynamic modeling and control of large flexible spacecraft combination. Scientia Sinica Physica, Mechanica & Astronomica, 2019,42(2):62-73 (in Chinese)) | | [10] | 缪炳祺, 曲广吉. 采用系统模态时柔性航天器的混合坐标动力学方程. 航天器工程, 1998,7(3):39-44 | | [10] | ( Miao Bingqi, Qu Guangji. Mixed coordinate dynamic equation of flexible spacecraft with system mode. Spacecraft Engineering, 1998,7(3):39-44 (in Chinese)) | | [11] | 刘伦. 航天器姿态运动与太阳翼结构振动耦合分析及协同控制. [博士论文]. 哈尔滨:哈尔滨工业大学, 2017 | | [11] | ( Liu Lun. Coupled analysis and cooperative control for spacecraft attitude motion and solar panel vibration. [PhD Thesis]. Harbin: Harbin Institute of Technology, 2017 (in Chinese)) | | [12] | 袁秋帆, 王超磊, 齐乃明 等. 单翼大挠性航天器全局模态动力学建模及试验. 宇航学报, 2019,40(4):369-377 | | [12] | ( Yuan Qiufan, Wang Chaolei, Qi Naiming, et al. Global dynamic modeling for a spacecraft with single large flexible structure and experimental study. Journal of Astronautics, 2019,40(4):369-377 (in Chinese)) | | [13] | 朱孟萍, 耿磊, 陈新龙 等. 带有阻尼机构的多柔体航天器动力学建模. 空间控制技术与应用, 2017,43(3):34-40 | | [13] | ( Zhu Mengping, Geng Lei, Chen Xinlong, et al. Dynamic modeling of flexible multi-body spacecraft with damping mechanism. Aerospace Control and Application, 2017,43(3):34-40 (in Chinese)) | | [14] | 黎凯, 张尧, 徐余军. 柔性空间机械臂在轨操作仿真与分析. 空间控制技术与应用, 2018,44(5):60-69 | | [14] | ( Li Kai, Zhang Yao, Xu Yujun. Simulation and analysis of on-orbit operations with flexible space manipulators. Aerospace Control and Application, 2018,44(5):60-69(in Chinese)) | | [15] | 方柳, 刘玉亮, 赵桂平. 考虑动力刚化的挠性航天器的动力学建模与分析. 兵器装备工程学报, 2017,38(9):67-72 | | [15] | ( Fang Liu, Liu Yuliang, Zhao Guiping. Dynamic modeling and analysis for flexible spacecraft with dynamic stiffening. Journal of Ordnance Equipment Engineering, 2017,38(9):67-72 (in Chinese)) | | [16] | 吕旺, 向明江, 叶文郁 等. 挠性卫星在轨非约束模态计算研究. 宇航学报, 2014,35(4):404-409 | | [16] | ( Lü Wang, Xiang Mingjiang, Ye Wenyu, et al. Research on calculation of on-orbit unconstrained modal of flexible satellite. Journal of Astronautics, 2014,35(4):404-409 (in Chinese)) | | [17] | 王首喆, 刘华清, 张庆展 等. 挠性充液航天器超近程逼近段动力学建模与控制. 中国空间科学技术, 2017,37(4):1-9 | | [17] | ( Wang Shouzhe, Liu Huaqing, Zhang Qingzhan, et al. Modeling and control for a liquid-filled spacecraft with flexible appendages in close proximity. Chinese Space Science and Technology, 2017,37(4):1-9 (in Chinese)) | | [18] | 孟得山. 柔性空间机器人操作大挠性航天器的动力学与振动控制. [博士论文]. 哈尔滨:哈尔滨工业大学, 2017 | | [18] | ( Meng Deshan. Dynamics and vibration control of a flexible space robot for manipulating a large flexible spacecraft. [PhD Thesis]. Harbin: Harbin Institute of Technology, 2017 (in Chinese)) | | [19] | 魏进, 曹登庆, 于涛. 复合柔性结构全局模态函数提取与状态空间模型构建. 力学学报, 2019,51(2):341-353 | | [19] | ( Wei Jin, Cao Dengqing, Yu Tao. Extraction of global mode functions and construction of state space model for a composite flexible structure. Chinese Journal of Theoretical and Applied Mechanics, 2019,51(2):341-353 (in Chinese)) | | [20] | 孙加亮, 田强, 胡海岩. 多柔体系统动力学建模与优化研究进展. 力学学报, 2019,51(6):1565-1586 | | [20] | ( Sun Jialiang, Tian Qiang, Hu Haiyan. Advances in dynamic modeling and optimization of flexible multibody systems. Chinese Journal of Theoretical and Applied Mechanics, 2019,51(6):1565-1586 (in Chinese)) | | [21] | 曹登庆, 白坤朝, 丁虎 等. 大型柔性航天器动力学与振动控制研究进展. 力学学报, 2019,51(1):1-13 | | [21] | ( Cao Dengqing, Bai Kunchao, Ding Hu, et al. Advances in dynamics and vibration control of large-scale flexible spacecraft. Chinese Journal of Theoretical and Applied Mechanics, 2019,51(1):1-13 (in Chinese)) | | [22] | Barbieri E. Unconstrained and constrained mode expansions for a flexible slewing link. Transaction of ASME, 1998,110(6):416-421 | | [23] | Hablani HB. Constrained and unconstrained modes: some modeling aspects of flexible spacecraft. Journal of Guidance, Control and Dynamics, 1982,5(2):164-173 | | [24] | 陕晋军, 关英姿, 王凤鸣 等. 挠性结构的约束模态及非约束模态解法. 上海航天, 2000,17(5):19-22,27 | | [24] | ( Shan Jinjun, Guan Yingzi, Wang Fengming, et al. Solution of constrained mode and unconstrained mode of flexible structure. Aerospace Shanghai, 2000,17(5):19-22,27 (in Chinese)) | | [25] | 缪炳祺, 施高萍, 黄欢. 多柔体系统动力学建模中部件模态的选择. 工程设计学报, 2004,11(4):205-210 | | [25] | ( Miao Bingqi, Shi Gaoping, Huang Huan. Selection of component modes for multi-flexible system. Journal of Engineering Design, 2004,11(4):205-210 (in Chinese)) | | [26] | Hughes PC. Modal identities for elastic bodies with application to vehicle dynamic and control. Journal Applied Mechanic, 1980,47(1):177-184 | | [27] | Hughes PC, Skelton RE. Modal truncation for flexible spacecraft. Journal of Guidance, Control and Dynamics, 1981,4(3):291-297 | | [28] | 罗文. 太阳翼卫星的刚柔藕合动力学建模. [硕士论文]. 哈尔滨:哈尔滨工业大学, 2015 | | [28] | ( Luo Wen. Rigid flexible coupling dynamic modeling of satellite with solar wings. [Master Thesis]. Harbin: Harbin Institute of Technology, 2015 (in Chinese)) | | [29] | Hablani HB. Modal identities for multibody elastic spacecraft. Journal of Guidance, Control and Dynamics, 1991,l4(2):294-303 | | [30] | 徐小胜, 于登云, 曲广吉. 用于惯性完备性降价的模态恒等式研究. 航天器工程, 2003,12(2):23-34 | | [30] | ( Xu Xiaosheng, Yu Dengyun, Qu Guangji. Modal identity for inertia completeness reduction. Spacecraft Engineering, 2003,12(2):23-34 (in Chinese)) | | [31] | 李东旭. 挠性航天器结构动力学. 北京: 科学出版社, 2010 | | [31] | ( Li Xudong. Structural Dynamics of Flexible Spacecraft. Beijing: Science Press, 2010 (in Chinese)) | | [32] | 王建明, 刘又午, 洪嘉振. 大范围刚体运动对柔性梁模态形函数的影响分析. 中国机械工程, 2000,11(6):49-51 | | [32] | ( Wang Jianming, Liu Youwu, Hong Jiazhen. Analysis on the mode shapes of flexible beams affected by large overall motion. China Mechanical Engineering, 2000,11(6):49-51 (in Chinese)) | | [33] | 施高萍, 缪炳棋. 基于部件模态的多柔体系统非约束频率估计. 浙江工业大学学报, 2004,32(3):260-265 | | [33] | ( Shi Gaoping, Miao Bingqi. Based on component modes estimate of the unconstrained frequencies of flexible multibody systems. Journal of Zhejiang University of Technology, 2004,32(3):260-265 (in Chinese)) |
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