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北京大学 [3]

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兰州理工大学 [2]

长春光学精密机械与物... [2]

光电技术研究所 [2]

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	Robust Graph Neural Networks Against Adversarial Attacks via Jointly Adversarial Training 会议论文上海, 2020-12-3 作者: Tian Hu; Ye Bowei; Zheng Xiaolong; Zhang Xingwei; Wu Dash Desheng 收藏 \| 浏览/下载：0/0 \| 提交时间：2023/07/04
	Perturbation Influences of Parameters on Dynamic Performance of a Virtual Synchronous Generator 会议论文 IECON 2017 - 43RD ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY, 2017-01-01 作者: Zhang, Lijun[1]; Wang, Fei[2]; Guo, Hui[3]; Feng, Xiayun[4]; Du, Yan[5] 收藏 \| 浏览/下载：6/0 \| 提交时间：2019/04/24 virtual synchronous generator (VSG) adaptive parameter virtual inertia small signal modeling
	Fourth-order Perturbed Eigenvalue Equation for Stepwise Damage Detection of Aeroplane Wing 会议论文作者: Wong, Chun Nam; Tang, Kongzheng; Jin, Wuyin; Tu, Gaoqiao 收藏 \| 浏览/下载：9/0 \| 提交时间：2019/11/15
	Lateral migration of fiber in settling suspensions 会议论文 Paper Conference and Trade Show, PaperCon 2014, Nashville, TN, United states, April 26, 2014 - April 30, 2014 作者: Qi DW; He GW(何国威); Liu YM 收藏 \| 浏览/下载：14/0 \| 提交时间：2017/05/27 Fiber aspect ratio Fiber suspensions Lateral migration Lattice Boltzmann simulations Particle densities Particle number density Repulsive forces Rotational inertia
	The study of 2+1 dimensional KdV equation in non-uniform dusty plasmas 会议论文作者: Zhang, Xi Jun; Xue, Jian Bin; Ma, Dong Lin; Zhang, Li Ping 收藏 \| 浏览/下载：24/0 \| 提交时间：2020/11/15 Ionization of gases Nonlinear equations Plasma theory Semiconductor plasmas Solitons Wave plasma interactions Dust charge fluctuation Dust-acoustic solitary waves Inhomogeneities Nonlinear properties Nonlinear solitary waves Reductive perturbation Transverse perturbation Variable coefficients
	Longitudinal control law design and simulation of fixed-wing UAV (EI CONFERENCE) 会议论文 2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China Duan Z. 收藏 \| 浏览/下载：19/0 \| 提交时间：2013/03/25 Taken some fixed-wing UAV as the study object the aircraft movement was broken down into the longitudinal movement and lateral movement according to the linearized small perturbation principle the longitudinal control law design method was discussed using root locus which belonged to classical control theory. The six degrees of freedom nonlinear model simulation result shows that: the control parameters designed are reasonable the simulation profile is fully consistent with the setting profile the control effect of pitch angle loop and altitude loop meets with the indices requirements the method is mature and reliable easy to realize in engineering. (2013) Trans Tech Publications Switzerland.
	Longitudinal control law design and simulation of fixed-wing UAV 会议论文 2012 International Conference on Measurement, Instrumentation and Automation, ICMIA 2012, September 15, 2012 - September 16, 2012, Guangzhou, China, September 15, 2012 - September 16, 2012 Duan Z. 收藏 \| 浏览/下载：15/0 \| 提交时间：2014/05/15
	Rotating Stall Inception in Axial Compressors under Periodic Perturbations 会议论文 Dong, Wanjing; Wang, Yong 收藏 \| 浏览/下载：2/0 \| 提交时间：2015/11/13 Moore-Greitzer Model Rotating Stall Periodical Perturbation Normal Form HIGH-SPEED STAGE INLET DISTORTION TRANSIENTS STABILITY SYSTEMS
	Sensor fault-tolerance control of a flexible air-breathing hypersonic flight vehicle 会议论文 Lei, Zhengdong; Yang, Jianying; Zhao, Yangyang 收藏 \| 浏览/下载：2/0 \| 提交时间：2015/11/13
	Influencing Factors on Dynamic Response of Hydrostatic Guideways 会议论文作者: Wang, Zhiwei; Zhao, Wanhua; Lu, Bingheng 收藏 \| 浏览/下载：3/0 \| 提交时间：2019/12/10 Settling time Dynamic. response Hydrostatic guideways Small perturbation method Reynolds equation

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