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个人信息Personal Information
教授
博士生导师
硕士生导师
性别：男
毕业院校：大连理工大学
学位：博士
所在单位：力学与航空航天学院
学科：动力学与控制. 航空航天力学与工程. 飞行器设计
联系方式：壹叁肆柒捌玖柒壹零玖肆
电子邮箱：tansj@dlut.edu.cn
扫描关注
- [21]Tan, Shu-Jun, Peng, Hai-Jun, Zhou, Wen-Ya, Wu, Zhi-Gang, WY (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian, Peoples R China..A novel extended precise integration method based on Fourier series expansion for the H-2-norm ...[J],INTERNATIONAL JOURNAL OF CONTROL,2016,89(10):2083-2095
- [22]王庆伟, 谭述君, 吴志刚, 杨云飞, 于子文, Tan, Shu-Jun.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
- [23]Tan, Shujun, Wang, Qingwei, Wu, Zhigang, ZG (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, State Key Lab Struct Anal Ind Equipment, 2 Linggong Rd, Dalian 116024, Peoples R China..Effects of Damping Ratio and Critical Coupling Strength on Pogo Instability[J],JOURNAL OF SPACECRAFT AND ROCKETS,2016,53(2):370-379
- [24]高强, 谭述君, 钟万勰, Gao, Qiang(qgao@dlut.edu.cn).精细积分方法研究综述[J],中国科学. 技术科学,2016,46(12):1207-1218
- [25]彭海军, 谭述君, 李云鹏, 陈飙松.An Improved Time-varying Controller based on Parameter Optimization for Libration-Point Orbit Mai...[J],ASCE Journal of Aerospace Engineering,2016,29(1):1-13
- [26]Ni, Zhiyu, Tan, Shujun, Wu, Zhigang, ZG (reprint author), Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China., Wu, Sch Aeronaut & Astronaut.Identification of Time-varying Frequencies and Model Parameters for Large Flexible On-orbit Sat...[J],TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES,2016,59(3):150-160
- [27]Yang, Chunfeng, Peng, Haijun, Tan, Shujun, Li, Yunpeng, Chen, Biaosong, HJ (reprint author), Dalian Univ Technol, Dept Engn Mech, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China..Improved Time-Varying Controller Based on Parameter Optimization for Libration-Point Orbit Main...[J],JOURNAL OF AEROSPACE ENGINEERING,2016,29(1)
- [28]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
- [29]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
- [30]倪智宇, 谭述君, 吴志刚, Wu, Zhi-Gang(wuzhg@dlut.edu.cn).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
- [31]谭述君, 吴志刚, 穆瑞楠.重力梯度对超大柔性空间结构在轨动力学特性的影响[A],2015,118-118
- [32]倪智宇, 谭述君, 吴志刚, Wu, Zhi-Gang(wuzhg@dlut.edu.cn).线性时变反馈系统的状态空间模型和模态参数递推辨识[J],控制与决策,2015,31(2):324-330
- [33]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
- [34]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],2015,236-236
- [35]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],2015,236-237
- [36]倪智宇, 邬树楠, 吴志刚, 谭述君, Wu, Zhi-Gang(wuzhg@dlut.edu.cn).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
- [37]谭述君, 王庆伟, 吴志刚, Tan, Shu-Jun.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
- [38]Lan, Lan, Fang, Houfei, Zhou, Yang, Wu, Zhigang, Tan, Shujun, Jiang, Shuidong.Geometry adaptive control of a composite reflector using PZT actuator[A],2015,9433
- [39]Wang, Qingwei, Yang, Yunfei, Yu, Ziwen, Tan, Shujun, Wu, Zhigang, SJ (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian 116024, Peoples R China..Improved modelling method of Pogo analysis and simulation for liquid rockets[J],ACTA ASTRONAUTICA,2015,107:262-273
- [40]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