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蒋建平

蒋建平,新万博代理方式教授、博士生导师,主要从事柔性航天器动力学与智能控制、智能结构及其在振动控制中应用、超静超稳航天器平台结构技术等研究,作为负责人或核心成员,承担或参与完成了重大科研项目10余项,曾获国家级科技进步奖、技术发明奖各1项。兼任中国指挥与控制学会空天安全平行系统专业委员会常务委员、湖南省力学学会理事等。
近期承担科研项目旨在探索柔性航天器动力学模拟新方法、基于智能材料航天结构振动控制技术,解决复杂航天器动力学姿态/轨道/结构的耦合动力学分析、航天器智能结构振动控制等难题。热忱欢迎申报或报考硕士生、博士生、直博生,热忱欢迎有志学友申请博士后、专职科研等岗位。
电子邮箱:jianping202@163.com
 
基本信息
蒋建平,男,39岁,四川广安人,1998~2009年就读于国防科技大学,先后获学士、硕士和航空宇航科学与技术博士学位,现任新万博代理方式教授,博士生导师。
工作经历
2018.05至今 新万博代理方式教授、博士生导师
2012.12–2017.11 国防科学技术大学航天科学与工程学院 副教授
2009.12–2011.11 国防科学技术大学航天与材料工程学院 讲师
2016.06–2016.12 英国斯旺西大学工程学院 访问学者
主要荣誉
2017年 军队科技进步二等奖,排名第6
2014年 国家科技进步二等奖,排名第2
2012年 军队科技进步一等奖,排名第5
2010年 国家技术发明二等奖,排名第2
2009年 军队科技进步一等奖,排名第2
2012年 博士论文被评为全国优秀博士学位论文
2012年 荣立二等功1次
2010年 荣立三等功1次
研究方向
1、柔性航天器动力学与智能控制
2、智能结构动力学及其振动控制
3、航天器微振动分析与控制技术
科研情况
作为项目负责人,承担并完成了国家自然科学基金、(原)总装武器装备预研、国防973项目子课题、科工局民用航天预研等各类项目10余项。作为核心技术骨干,参与完成了国家“高分”重大专项项目2项、(原)总装武器装备预研项目2项、国家863项目3项。获国家技术发明二等奖1项(排名2)、国家科技进步二等奖1项(排名2)、军队科技进步一等奖2项(排名2、5)、军队科技进步二等奖1项(排名6),获授权发明专利15项,发表学术论文40余篇,其中SCI检索30余篇。
学术任职
1、湖南省力学学会理事
2、中国指挥与控制学会空天安全平行系统专业委员会常务委员
3、担任多个SCI期刊审稿人
1) Smart Materials and Structures
2) Journal of Sound and Vibration
3) International Journal of Applied Mechanics
4) Aerospace Science and Technology
5) Journal of Intelligent Material Systems and Structures
6) IEEE Transactions on Control Systems Technology
部分论文
[1] Wang J, Li D, Jiang J. First order coupled dynamic model of flexible space structures with time-varying configurations[J]. Acta Astronautica, 2017, 132:117-123.
[2] Wang J, Li D, Jiang J. Optimal Variable Amplitudes Input Shaping Control for Slew Maneuver of Flexible Spacecraft[J]. Journal of Guidance Control & Dynamics, 2017, 40(6).
[3] Wang J, Li D, Jiang J. Modeling and Analysis of Coupled Flexural-Torsional Spinning Beams with Unsymmetrical Cross Sections[J]. Journal of Theoretical & Applied Mechanics, 2017, 55(1):213.
[4] Rui X U, Dong-Xu L I, Jiang J P. Decentralized Adaptive Fuzzy Vibration Control of Smart Solar Panel[C]// International Conference on Artificial Intelligence Science and Technology. 2017:65-74.
[5] Wang B, Li D X, Jiang J P, et al. A judging principle of crucial vibrational transmission paths in plates[J]. Journal of Sound & Vibration, 2016, 380:146-164.
[6] Luo Q, Li D, Jiang J. Analysis and Optimization of Microvibration Isolation for Multiple Flywheel Systems of Spacecraft[J]. Aiaa Journal, 2016, 54(5):1-13.
[7] Wang J, Li D, Jiang J. Integrated Control of Thermally Induced Vibration and Quasi-Static Deformation of Space Truss[J]. Journal of Dynamic Systems Measurement & Control, 2016, 138(8).
[8] Wang J, Li D, Jiang J. Thermally induced deformation of ultra-large truss support membrane structure[J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2016, 231(13).
[9] Xu R, Li D X, Jiang J, et al. Decentralized adaptive fuzzy vibration control of smart gossamer space structure[J]. Journal of Intelligent Material Systems & Structures, 2016, 28(12).
[10] Xu R, Li D, Jiang J. Online learning fuzzy vibration control of smart truss structure[J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2016, 231(3).
[11] Wang B, Li D X, Jiang J P, et al. A modified firefly algorithm based on light intensity difference[J]. Journal of Combinatorial Optimization, 2016, 31(3):1045-1060.
[12] Wei Z, Li D, Luo Q, Jiang J P. Performance Analysis of a Flywheel Microvibration Isolation Platform for Spacecraft[J]. Journal of Spacecraft & Rockets, 2015, 52(4):1-6.
[13] Wei Z, Li D, Luo Q, Jiang J P. Modeling and analysis of a flywheel microvibration isolation system for spacecrafts[J]. Advances in Space Research, 2015, 55(2):761-777.
[14] Xu R, Li D X, Luo Q, Jiang J P. Microvibration suppression of space truss structures using viscoelastic dampers with design parameter optimization[J]. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2015, 230(3).
[15] Xu R, Li D X, Liu W, Jiang J P. Modified nonlinear force density method for form-finding ofmembrane SAR antenna[J]. Structural Engineering & Mechanics, 2015, 54(6):1045-1059.
[16] Xu R, Li D, Jiang J. An online learning-based fuzzy control method for vibration control of smart solar panel[J]. Journal of Intelligent Material Systems & Structures, 2015, 26(18).
[17] Wang J, Li D, Jiang J. Coupled flexural–torsional vibration of spinning smart beams with asymmetric cross sections[J]. Finite Elements in Analysis & Design, 2015, 105(1):16-25.
[18] Li D, Jiang J, Liu W, et al. A New Mechanism for the Vibration Control of Large Flexible Space Structures With Embedded Smart Devices[J]. IEEE/ASME Transactions on Mechatronics, 2015, 20(4):1653-1659.
[19] Luo Q, Li D, Jiang J. Coupled dynamic analysis of a single gimbal control moment gyro cluster integrated with an isolation system[J]. Journal of Sound & Vibration, 2014, 333(2):345-363.
[20] Jie W, Li D, Jiang J, et al. Thermal Analysis of Large Deployable Truss Support Membrane Structure on Satellite[J]. Bulletin of Surveying & Mapping, 2014, s0:9-14.
[21] Jiang J P, Rui X U. Dynamic Modeling and Vibration Control for Spacecraft's Solar Array[C]// International Conference on Mechanics and Civil Engineering. 2014.
[22] Liu W, Li D, Jiang J. General Mesh Configuration Design Approach for Large Cable-Network Antenna Reflectors[J]. Journal of Structural Engineering, 2014, 140(2):441-454.
[23] Liu W, Li D X, Yu X Z, Jiang J P. Exact mesh shape design of large cable-network antenna reflectors with flexible ring truss supports[J]. Acta Mechanica Sinica, 2014, 30(2):198-205.
[24] Jiang J P, Xu R. Dynamic Modeling and Vibration Control for Spacecraft’s Solar Array[J]. Atlantis Press, 2014.
[25] Li D, Luo Q, Jiang J, et al. Dynamic modelling and observation of micro-vibrations generated by a Single Gimbal Control Moment Gyro[J]. Journal of Sound & Vibration, 2013, 332(19):4496-4516.
[26] Zhou W Y, Li D X, Luo Q, Jiang J P. Design and test of a soft suspension system for cantilevered momentum wheel assembly[J]. Proceedings of Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, 2013, 227(7):1144-1160.
[27] Jiang J P, Liu W, Li D X. Mesh topological form design and geometrical configuration generation for cable-network antenna reflector structures[J]. Structural Engineering & Mechanics, 2013, 45(3):411-422.
[28] Li D X, Liu W, Jiang J P. Optimal Placement of Controls for Truss Structures in Space[M]. IEEE Educational Activities Department, 2012.
[29] Li D X, Liu W, Jiang J P. Optimal Placement of Controls for Truss Structures in Space[M]. IEEE Educational Activities Department, 2012.
[30] Jiang J P, Li D X. Robust H ∞ vibration control for smart solar array structure[J]. Journal of Vibration & Control, 2011, 17(4):505-515.
[31] Li D, Liu W, Jiang J P. GA-based Optimal Placement of Sensors and Actuators for Space Intelligent Truss Structures[J].  2011.
[32] Li D X, Liu W, Jiang J P. The influence of orbital motion of flexible space vehicle on the dynamic traits of solar panel[C]// International Conference on Communications, Computing and Control Applications. IEEE, 2011:1-5.
[33] Jiang J P, Li D X. Decentralized Robust Vibration Control of Smart Structures with Parameter Uncertainties[J]. Journal of Intelligent Material Systems & Structures, 2011, 22(2):137-147.
[34] Li D X, Liu W, Jiang J P, et al. Placement optimization of actuator and sensor and decentralized adaptive fuzzy vibration control for large space intelligent truss structure.[J]. Science China, 2011, 54(4):853-861.
[35] Jiang J, Li D. Optimal placement and decentralized robust vibration control for spacecraft smart solar panel structures[J]. Smart Materials & Structures, 2010, 19(8):085020.
[36] Jiang J P, Li D X. Decentralized guaranteed cost static output feedback vibration control for piezoelectric smart structures[J]. Smart Materials & Structures, 2010, 19(1):015018.
[37] Jiang J, Li D. Finite element formulations for thermopiezoelastic laminated composite plates[J]. Smart Materials & Structures, 2008, 17(17):015027.
[38] Jiang J, Li D. A Higher Order Theory for Piezoelectric Plate[C]// The World Forum on Smart Materials and Smart Structures Technology. 重庆大学, 2007.
[39] Jiang J, Dongxu L I. Research on Rigid-Flexible Coupling Dynamics of Spacecraft with Solar Panel[J]. Acta Aeronautica Et Astronautica Sinica, 2006, 27(3):418-422.