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Huang YongAn
Professor
Supervisor of Doctorate Candidates Supervisor of Master's Candidates
Professional Title:
Professor
Gender:
Male
Status:
Employed
Department:
智能制造装备与技术全国重点实验室
Education Level:
Postgraduate (Doctoral)
Degree:
Doctoral Degree in Engineering
Alma Mater:
Northwestern Polytechnical University
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Paper Publications
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Paper Publications
黄永安,黄永安; 尹周平; 邓子辰; 熊有伦.多体动力学的几何积分方法研究进展.[J].力学进展,2009,(1):44-57
Huang YongAn,Huang YongAn ; Yin Zhouping; Hu Xiangtao; Xiong Youlun.A Novel Force Control Method for Quasi-Static Underactuated Multibody Systems.[J].Advanced Robotics,2008,(10):1249-1260
Huang YongAn,Huang YongAn ; Xiong Youlun.Force Planning for Underground Articulated Robot.[J].1st International Conference on Intelligent Robotics and Applications,
Huang, YongAn, YongAn ; Deng, Zichen; Xiong, Youlun.High-order model and slide mode control for rotating flexible smart structure.Mechanism and Machine Theory,2008,(8):1038-1054
Huang YongAn,Huang YongAn ; Yin Zhouping; Xiong Youlun.Modeling and Computation for the High-Speed Rotating Flexible Structure.Journal of Vibration and Acoustics-Transactions of the ASME,2008,(4):041005
Huang YongAn ; Deng Zichen,Huang YongAn ; Deng Zichen ; Yao Linxiao.Dynamic analysis of a rotating rigid-flexible coupled smart structure with large deformations.Applied Mathematics and Mechanics (English Edition ),2007,(10):1349-1360
Yong-An Huang, Zi-Chen Deng, Wen-Cheng Li.Sliding mode control based on neural network for the vibration reduction of flexible structures.Structural Engineering and Mechanics,2007,(4):377-392
Yong-an Huang, Zi-chen Deng, Lin-xiao Yao.An improved symplectic precise integration method for analysis of the rotating rigid-flexible coupled system.Journal of sound and vibration,2007,(1-2):229-246
Li Wen-cheng (李文成),Li Wen-cheng (李文成)Deng Zi-chen (邓子辰)Huang Yong-an (黄永安).Efficient numerical integrators for highly oscillatory dynamic systems based on modified magnus integrator method.Applied Mathematics and Mechanics,2006,(10):1383-1390
YA Huang, ZC Deng.Decentralized Sliding Mode Control for a Spacecraft Flexible Appendage Based on Finite Element Method.2005,(3):230-236
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