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[1]Zhang, Jie,Peng, Haijun,Zhou, Wenya,Yang, Jinzhao,Wu, Zhigang.Dynamic modeling and verification of continuum robot based on cable drive[A],2019,262-267
[2]Ni, Zhiyu,Liu, Jinguo,Wu, Shunan,Wu, Zhigang.Time-varying state-space model identification of an on-orbit rigid-flexible coupling spacecraft using an improved predictor-based recursive subspace algorithm[J],ACTA ASTRONAUTICA,2019,163(,SI):157-167
[3]Ni, Zhiyu,Liu, Jinguo,Wu, Shunan,Wu, Zhigang.TIME-VARYING STATE-SPACE MODEL IDENTIFICATION OF ON-ORBIT RIGID-FLEXIBLE COUPLING SPACECRAFT USING A PREDICTOR-BASED RECURSIVE SUBSPACE ALGORITHM[A],2018,165:981-994
[4]Song, Xiangshuai,Tan, Shujun,Wang, Enmei,Wu, Shunan,Wu, Zhigang.Active shape control of an antenna reflector using piezoelectric actuators[J],JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES,2019,30(18-19):2733-2747
[5]Wang, Enmei,Wu, Shunan,Song, Xiangshuai,Wu, Zhigang,Liu, Yufei.DISTRIBUTED COOPERATIVE VIBRATION CONTROL FOR THE SOLAR POWER SATELLITE[A],2018,165:877-886
[6]Mu, Ruinan,Wu, Shunan,Radice, Gianmarco,Wu, Zhigang,Qi, Zhaohui.INTEGRATED ATTITUDE CONTROL OF SOLAR POWER SATELLITE BASED ON ELECTRIC PROPULSION AND MOVING MASS SYSTEM[A],2018,165:861-875
[7]Wu, Shunan,Wen, Shenghui,Ma, Xue,Wu, Zhigang.AN ELECTRIC-PROPULSION-BASED MERCURY ORBIT TRANSFER STRATEGY SUBJECT TO THIRD-BODY PERTURBATION[A],2018,165:1705-1713
[8]王晓明,周文雅,吴志刚,张小虎.Integrated design of laminated composite structures with piezocomposite actuators for active shape control[J],Composite Structures, 2019,215(2019): 166-177,2019,215:166-177
[9]倪智宇,刘金国,吴志刚.一种改进的航天器时变模态参数递推辨识方法[J],宇航学报,2018,39(10):1097-1106
[10]Wu, Shunan,Chu, Weimeng,Ma, Xue,Radice, Gianmarco,Wu, Zhigang.Multi-objective integrated robust H infinity control for attitude tracking of a flexible spacecraft[J],ACTA ASTRONAUTICA,2018,151:80-87
[11]穆瑞楠,谭述君,吴志刚,齐朝晖.超大柔性空间结构姿态振动耦合稳定性分析[J],宇航学报,2018,39(7):709-714
[12]Mu, Ruinan,Tan, Shujun,Wu, Zhigang,Qi, Zhaohui.Coupling dynamics of super large space structures in the presence of environmental disturbances[J],ACTA ASTRONAUTICA,2018,148:385-395
[13]穆瑞楠,王艺睿,谭述君,吴志刚,齐朝晖.空间太阳能电站姿态运动-结构振动耦合建模与分析[J],宇航学报,2018,39(6):615-623
[14]Wang, Xiaoming,Zhou, Wenya,Wu, Zhigang,Wu, Wenhua.Optimal unimorph and bimorph configurations of piezocomposite actuators for bending and twisting vibration control of plate structures[J],JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES,2018,29(8):1685-1696
[15]Wang, Xiaoming,Zhou, Wenya,Wu, Zhigang.Feedback tracking control for dynamic morphing of piezocomposite actuated flexible wings[J],JOURNAL OF SOUND AND VIBRATION,2018,416:17-28
[16]Wang, Xiaoming,Zhou, Wenya,Xun, Guangbin,Wu, Zhigang.Dynamic shape control of piezocomposite-actuated morphing wings with vibration suppression[J],JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES,2018,29(3):358-370
[17]谭述君,王庆伟,吴志刚,杨云飞,于子文.A method for deriving a non-singular state-space formulation based on Rubin's model for Pogo analysis[J],Proceedings of the Institution of Mechanical Engineering Part G-Journal of Aerospace Engineering,2018
[18]宋祥帅,谭述君,吴志刚,兰澜.格栅反射器型面闭环主动控制实验研究[A],第三届可展开空间结构学术会议,2018
[19]寻广彬,谭述君,吴志刚,兰澜.索网天线反射面索网生成的准等边三角形网格法[A],第三届可展开空间结构学术会议,2018
[20]刘玉亮,邬树楠,刘家夫,吴志刚.空间太阳能电站重力姿态-轨道-结构耦合特性[J],航空学报,2017,38(12):154-165
[21]Tan, Shu-Jun,Zhou, Wen-Ya,Peng, Hai-Jun,Wu, Zhi-Gang.A novel extended precise integration method based on Fourier series expansion for periodic Riccati differential equations[J],OPTIMAL CONTROL APPLICATIONS & METHODS,2017,38(6):896-907
[22]Liu, Yuliang,Wu, Shunan,Zhang, Kaiming,Wu, Zhigang.Parametrical Excitation Model for Rigid-Flexible Coupling System of Solar Power Satellite[J],JOURNAL OF GUIDANCE CONTROL AND DYNAMICS,2017,40(10):2674-2681
[23]何骁,谭述君,吴志刚.大角度机动下带挠性附件航天器转动惯量在轨辨识[J],宇航学报,2017,38(9):927-935
[24]初未萌,邬树楠,吴志刚.航天器状态测量的智能降噪方法[A],第十届全国多体动力学与控制暨第五届全国航天动力学与控制学术会议,2017,1
[25]文生辉,马雪,邬树楠,吴志刚.水星环绕轨道的电推进变轨控制方法[A],第十届全国多体动力学与控制暨第五届全国航天动力学与控制学术会议,2017,1
[26]宋祥帅,谭述君,吴志刚.格栅反射器主动型面控制研究[A],第十届全国多体动力学与控制暨第五届全国航天动力学与控制学术会议,2017,1
[27]王恩美,邬树楠,吴志刚.空间太阳能电站在轨组装过程中的分布式振动控制[A],第十届全国多体动力学与控制暨第五届全国航天动力学与控制学术会议,2017,1
[28]谭述君,陈宇,王庆伟,吴志刚.POGO回路建模新方法及稳定性分析[A],中国力学大会-2017暨庆祝中国力学学会成立60周年大会,2017,13
[29]穆瑞楠,谭述君,吴志刚.重力梯度对超大柔性空间结构在轨动力学特性的影响[J],国防科技大学学报,2017,39(3):7-14
[30]兰聪超,谭述君,吴志刚,李文博.带挠性附件卫星转动惯量的在轨辨识[J],振动与冲击,2017,36(8):16-21,33
[31]Liu, Yuliang,Wu, Shunan,Zhang, Kaiming,Wu, Zhigang.Gravitational orbit-attitude coupling dynamics of a large solar power satellite[J],AEROSPACE SCIENCE AND TECHNOLOGY,2017,62:46-54
[32]王晓明,周文雅,寻广彬,吴志刚.带有振动抑制的压电结构动态形状主动控制[J],宇航学报,2017,38(2):185-191
[33]Ni, Zhiyu,Wu, Zhigang,Liu, Jinguo,Shen, Xinhui.On-orbit Identification of Time-varying Moment of Inertia for Spacecraft Based on a Recursive Subspace Method[A],PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017),2017,2133-2138
[34]周文雅,吴志刚.压电驱动的柔性机翼形状主动控制技术研究[A],2017
[35]Peng, Haijun,Tan, Shujun,Gao, Qiang,Wu, Zhigang.Symplectic method based on generating function for receding horizon control of linear time-varying systems[J],EUROPEAN JOURNAL OF CONTROL,2017,33:24-34
[36]王晓明,吴志刚,周文雅.压电驱动柔性机翼的开环轨迹跟踪控制[A],2016年航空科学与技术全国博士生学术论坛,2016,2
[37]Tan, Shu-Jun,Peng, Hai-Jun,Zhou, Wen-Ya,Wu, Zhi-Gang.A novel extended precise integration method based on Fourier series expansion for the H-2-norm of linear time-varying periodic systems[J],INTERNATIONAL JOURNAL OF CONTROL,2016,89(10):2083-2095
[38]周文雅,邢健,罗阳军,王晓明,吴志刚.面向大展弦比机翼振动抑制的作动器优化配置[A],第35届中国控制会议,2016,6
[39]Wu, Shunan,Zhang, Kaiming,Peng, Haijun,Wu, Zhigang,Radice, Gianmarco.Robust optimal sun-pointing control of a large solar power satellite[J],ACTA ASTRONAUTICA,2016,127:226-234
[40]刘玉亮,邬树楠,吴志刚,侯欣宾,刘宇飞.空间太阳能电站地球同步拉普拉斯轨道动力学特性[J],中国空间科学技术,2016,36(5):1-8
[41]寻广彬,吴志刚,彭海军,穆瑞楠,邬树楠.大型索网天线机电耦合动力学建模与主动变形控制[J],计算力学学报,2016,33(4):570-575
[42]吴志刚,刘玉亮,张开明,邬树楠.高阶重力和力矩对空间太阳能电站运动的影响[J],空间控制技术与应用,2016,42(4):1-5,35
[43]寻广彬,彭海军,邬树楠,吴志刚.非线性最小二乘跟踪的对偶变量变分方法[J],力学学报,2016,48(5):1202-1207
[44]彭海军,李飞,高强,陈飙松,吴志刚,钟万勰.多体系统轨迹跟踪的瞬时最优控制保辛方法[J],力学学报,2016,48(4):784-791
[45]Wang, Xiaoming,Zhou, Wenya,Wu, Zhigang,Xing, Jian.Tracking control system design for roll maneuver via active wings using macro fiber composites[A],AIAA Modeling and Simulation Technologies Conference, 2016,2016
[46]Ni, Zhiyu,Wu, Zhigang,Wu, Shunan.Time-varying modal parameters identification of large flexible spacecraft using a recursive algorithm[J],INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES,2016,17(2):184-194
[47]王庆伟,谭述君,吴志刚,杨云飞,于子文.大型液体火箭结构纵横扭振动与推进系统耦合(POGO)稳定性分析[J],振动与冲击,2016,35(10):167-173
[48]彭海军,吴志刚,钟万勰.面向深空探测的计算最优控制辛数学方法[A],第十届全国动力学与控制学术会议,2016,31-32
[49]邬树楠,文生辉,吴志刚.考虑参数时变的挠性航天器姿态鲁棒H∞控制[A],第十届全国动力学与控制学术会议,2016,104-105
[50]文生辉,杨新茗,邬树楠,吴志刚.空间太阳能电站的长期轨道动力学分析[A],第十届全国动力学与控制学术会议,2016,30-31
[51]周文雅,王晓明,吴志刚.压电纤维复合材料驱动的悬臂板动态形状主动控制[A],第十届全国动力学与控制学术会议论文集中国力学学会,2016,32-32
[52]Wang X.,Wu Z.,Zhou W..Nonlinear aeroelastic analysis and control of airfoil section with control surface freeplay[J],ICIC Express Letters,2016,10(5):1151-1156
[53]Tan, Shujun,Wang, Qingwei,Wu, Zhigang.Effects of Damping Ratio and Critical Coupling Strength on Pogo Instability[J],JOURNAL OF SPACECRAFT AND ROCKETS,2016,53(2):370-379
[54]周文雅,王恩美,吴志刚.高可靠性再入轨迹快速规划方法[J],系统工程与电子技术,2016,38(8):1867-1872
[55]周文雅,吴志刚.压电纤维复合材料驱动的机翼动态形状控制[J],航空学报,2016,37(5):1-6
[56]邬树楠,吴志刚.Gravitational orbit-attitude coupling dynamics of a large solar power satellite[J],Aerospace Science and Technology,2016,62(3):46-54
[57]Ni, Zhiyu,Mu, Ruinan,Xun, Guangbin,Wu, Zhigang.Time-varying modal parameters identification of a spacecraft with rotating flexible appendage by recursive algorithm[J],ACTA ASTRONAUTICA,2016,118:49-61
[58]Wang, Yutao,Zhou, Wenya,Pang, Yan,Wu, Zhigang.An Improved Reentry Trajectory Planning Method for Common Aero Vehicle[A],IEEE Chinese Guidance, Navigation and Control Conference (CGNCC),2016,369-374
[59]吴志刚,杨今朝,彭海军,张朔.轨道预报的一种乘法保辛摄动方法[J],中国科学. 技术科学,2016,46(12):1232-1241
[60]Ni, Zhiyu,Tan, Shujun,Wu, Zhigang.Identification of Time-varying Frequencies and Model Parameters for Large Flexible On-orbit Satellites Using a Recursive Algorithm[J],TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES,2016,59(3):150-160
[61]Li, Mingwu,Peng, Haijun,Wu, Zhigang.Symplectic Irregular Interpolation Algorithms for Optimal Control Problems[J],INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS,2015,12(6)
[62]谭述君,周文雅,吴志刚.线性定常系统非齐次两点边值问题的扩展精细积分方法[J],应用数学和力学,2015,36(11):1145-1157
[63]Peng, Haijun,Gao, Qiang,Wu, Zhigang,Zhong, Wanxie.Symplectic algorithms with mesh refinement for a hypersensitive optimal control problem[J],INTERNATIONAL JOURNAL OF COMPUTER MATHEMATICS,2015,92(11):2273-2289
[64]侯健,谭述君,穆瑞楠,吴志刚.大型索网天线结构在轨变形分析及软件研发[J],计算机辅助工程,2015,24(5):47-52
[65]邬树楠,刘丽坤,汪锐,吴志刚.大型索网式可展开天线在轨高精度指向控制[J],宇航学报,2015,36(10):1140-1147
[66]倪智宇,谭述君,吴志刚.改进的TW-API方法及其在时变模态参数辨识中的应用[J],振动工程学报,2015,28(5):721-729
[67]谭述君,穆瑞楠,吴志刚.重力梯度对超大柔性空间结构在轨动力学特性的影响[A],第九届全国多体系统动力学暨第四届全国航天动力学与控制学术会议,2015,1
[68]彭海军,李明武,吴志刚.考虑碰撞避免的平动点附近航天器"松散"编队控制研究[A],2015中国力学大会论文集中国力学学会,2015,236-236
[69]刘玉亮,邬树楠,周文雅,吴志刚.两种空间太阳能电站的轨道动力学特性研究[A],2015,54-54
[70]邬树楠,张开明,谭述君,吴志刚,侯欣宾,刘宇飞.空间太阳能电站对日指向的时变LQR控制[A],2015中国力学大会,2015,236-236
[71]谭述君,王庆伟,吴志刚,杨云飞,陈宇.大型液体火箭"姿控-结构-推进"耦合动力学建模与分析[A],2015中国力学大会,2015
[72]彭海军,李明武,吴志刚.考虑碰撞避免的平动点附近航天器"松散"编队控制研究[A],2015中国力学大会,2015
[73]赵国威,吴志刚.大范围运动细长柔性空间结构动力学特性分析[J],计算力学学报,2015,32(4):512-517
[74]谭述君,王庆伟,吴志刚,杨云飞,陈宇.大型液体火箭"姿控-结构-推进"耦合动力学建模与分析[A],2015中国力学大会论文集中国力学学会,2015,236-237
[75]倪智宇,邬树楠,吴志刚,谭述君.利用改进TW-API方法在轨辨识挠性航天器时变模态参数[J],宇航学报,2015,36(7):769-776
[76]张志刚,齐朝晖,吴志刚.一种基于应变插值大变形梁单元的刚-柔耦合动力学分析[J],振动工程学报,2015,28(3):337-344
[77]Wu, Shunan,Wang, Rui,Radice, Gianmarco,Wu, Zhigang.Robust attitude maneuver control of spacecraft with reaction wheel low-speed friction compensation[J],AEROSPACE SCIENCE AND TECHNOLOGY,2015,43:213-218
[78]赵国威,吴志刚.稳态轴向变形对旋转运动悬臂梁弯曲频率的影响[A],第十五届全国非线性振动暨第十二届全国非线性动力学和运动稳定性学术会议,2015,2
[79]谭述君,王庆伟,吴志刚.临界阻尼比法在POGO振动稳定性分析中的适用性[J],宇航学报,2015,36(3):284-291
[80]Lan, Lan,Jiang, Shuidong,Zhou, Yang,Fang, Houfei,Tan, Shujun,Wu, Zhigang.Geometry adaptive control of a composite reflector using PZT actuator[A],SPIE Industrial and Commercial Applications of Smart Structures Technologies Conference,2015,9433
[81]Wang, Qingwei,Tan, Shujun,Wu, Zhigang,Yang, Yunfei,Yu, Ziwen.Improved modelling method of Pogo analysis and simulation for liquid rockets[J],ACTA ASTRONAUTICA,2015,107:262-273
[82]赵国威,吴志刚.应变能中耦合项对旋转悬臂梁振动频率的影响[J],力学学报,2015,47(2):362-366
[83]彭海军,吴志刚.平动点航天器编队构型重构的快速路径规划[A],2015
[84]谭述君,吴志刚,穆瑞楠.超大柔性空间结构的在轨动力学特性研究[A],2015,1-1
[85]谭述君,吴志刚.Improved modeling method of POGO analysis and simulation for liquid rockets[J],Acta Astronautica,2015,107(1):262-273
[86]谭述君,王庆伟,吴志刚.临界阻尼比法在液体火箭POGO振动稳定性分析中的适用性[J],宇航学报,2015,36(7):769-776
[87]Zhang, Zhigang,Qi, Zhaohui,Wu, Zhigang,Fang, Huiqing.A Spatial Euler-Bernoulli Beam Element for Rigid-Flexible Coupling Dynamic Analysis of Flexible Structures[J],SHOCK AND VIBRATION,2015,2015
[88]王庆伟,谭述君,吴志刚,杨云飞,陈宇.大型液体火箭姿控与跷振大回路耦合动力学建模与分析[J],力学学报,2015,47(5):789-798
[89]Zhou W.,Wang H.,Ma H.,Wu Z..Longitudinal reentry guidance based on receding horizon control[J],ICIC Express Letters,2015,9(2):461-468
[90]杜剑明,穆瑞楠,吴志刚.星载可展开天线指向精度分析及指向调整方法[A],2014年“可展开空间结构”学术会议,2014,18-18