DALIAN UNIVERSITY OF TECHNOLOGY
Login
中文
Home
Scientific Research
Research Projects
Published Books
Patents
Paper Publications
Research Field
Teaching Research
Teaching Achievement
Teaching Information
Teaching Resources
Awards and Honours
Other Rewards
Academic Honor
Scientific Awards
Enrollment Information
Student Information
My Album
Blog
Current position:
Home
>>
Scientific Research
谭述君
Personal Information
Professor Supervisor of Doctorate Candidates Supervisor of Master's Candidates
Scientific Research
Research Field
No content
Paper Publication...
More>>
王庆伟, 谭述君, 潘辉, 张青松, 王小军.液体火箭POGO振动缩聚模型研究[J],振动与冲击,2019,38(1):8-13,36
Song, Xiangshuai, Tan, Shujun, Wang, Enmei, Wu, Shunan, Zhigang, SJ (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian 116024, Peoples R China..Active shape control of an antenna reflector using piezoelectric actuators[J],JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES,2019,30(18-19):2733-2747
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
Mu, Ruinan, Tan, Shujun, Wu, Zhigang, Qi, Zhaohui, SJ (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China..Coupling dynamics of super large space structures in the presence of environmental disturbances[J],ACTA ASTRONAUTICA,2018,148:385-395
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
宋祥帅, 王恩美, 穆瑞楠, 谭述君, 兰澜.格栅反射器型面的主动控制[J],航空学报,2018,39(6):101-109
Patents
More>>
一种大角度机动下带挠性附件航天器转动惯量在轨辨识方法
卫星动力学参数在轨辨识与鲁棒控制仿真软件
运载火箭先进姿态控制系统设计软件
复杂系统传递函数bode图绘制软件[简称: CSTFP]1.0
液体火箭推进-结构-控制动力学耦合分析软件[简称: LRPSC]1.0
大型索网天线结构在轨变形分析与预测软件[简称: LFAS]1.0
Published Books
现代控制系统设计与仿真—使用PIMCSD工具箱
Research Projects
More>>
高精度主控伞天线研究, 企事业单位委托科技项目, 2016/07/31-2020/06/30, 结题
超大柔性空间结构在轨动力学分析与振动控制, 国家自然科学基金项目, 2015/08/18, 结题
罩式炉结构变形、强度校核分析与优化设计, 企事业单位委托科技项目, 2010/11/26, 结题
时变LQ/H∞最优控制系统的高精度保辛数值算法研究, 国家自然科学基金项目, 2010/09/25-2013/12/31, 结题
AEC控制系统测试设备底层软件开发合同, 企事业单位委托科技项目, 2018/01/10-2024/07/05, 结题
空间连续型机器人缠绕捕获目标过程动力学与控制及其辛算法, 国家自然科学基金项目, 2017/12/15-2022/04/18, 结题