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	Highly and Adaptively Undersampling Pattern for Pulmonary Hyperpolarized Xe-129 Dynamic MRI 期刊论文 OAI收割 IEEE TRANSACTIONS ON MEDICAL IMAGING, 2019, 卷号: 38, 期号: 5, 页码: 1240-1250 作者: Zhou, Xin; Ye, Chaohui; Sun, Xianping; Li, Haidong; Xie, Junshuai \| 收藏 \| 浏览/下载：95/0 \| 提交时间：2019/06/24 Highly and adaptively undersampling pattern (HUP) dynamic MRI hyperpolarized Xe-129 lung compressed sensing (CS)
	TARCS: A Topology Change Aware-Based Routing Protocol Choosing Scheme of FANETs 期刊论文 OAI收割 ELECTRONICS, 2019, 卷号: 8, 期号: 3, 页码: 274 作者: Hong, Jie; Zhang, Dehai \| 收藏 \| 浏览/下载：109/0 \| 提交时间：2019/06/26 flying ad hoc network (FANET) mobile ad hoc network (MANET) highly dynamic periodical topology change awareness routing protocol
	Adaptive Optimal Control of Highly Dissipative Nonlinear Spatially Distributed Processes With Neuro-Dynamic Programming 期刊论文 OAI收割 IEEE TRANSACTIONS ON NEURAL NETWORKS AND LEARNING SYSTEMS, 2015, 卷号: 26, 期号: 4, 页码: 684-696 作者: Luo, Biao; Wu, Huai-Ning; Li, Han-Xiong 收藏 \| 浏览/下载：26/0 \| 提交时间：2016/03/30 Adaptive optimal control empirical eigenfunction (EEF) highly dissipative partial differential equations (PDEs) neuro-dynamic programming (NDP) spatially distributed processes (SDPs)
	资讯类新闻套图系统期刊论文 OAI收割计算机系统应用, 2014, 期号: 10, 页码: 57-62 江浩亮; 左春 \| 收藏 \| 浏览/下载：26/0 \| 提交时间：2014/12/16 Web信息提取动态数据集高可扩展性个性化推荐套图 web information extraction dynamic data set highly scalable personalized recommendations imgset
	A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏 \| 浏览/下载：67/0 \| 提交时间：2013/03/25 In this paper a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime but not accurate enough in the supersonic regime. 2011 IEEE.
	The study of two FOG filter methods in improving the precision of servo control system (EI CONFERENCE) 会议论文 OAI收割 2010 3rd International Conference on Advanced Computer Theory and Engineering, ICACTE 2010, August 20, 2010 - August 22, 2010, Chengdu, China 作者: Zhang Y.; Zhang L.-G.; Zhang L.-G. 收藏 \| 浏览/下载：18/0 \| 提交时间：2013/03/25 The precision of FOG has highly effect on the servo system's final precision. In this paper two filter methods has been researched in signal processing of FOG smoothing filter method and Kalman filter based on ARMA model in order to improve turn table servo control system's performance. To validate the effects of these two methods three experiments have been made which are filter examinations dynamic experiments and Static experiments. The experiments reveal that these two kinds of filter methods are useful to filter the unknown noises and very effective to improve the precision of servo control system. 2010 IEEE.