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Adaptive Fault-Tolerant Optimized Platoon Cloud Tracking Control for Heterogeneous Vehicles via Dual Learning Mechanism 期刊论文  OAI收割
IEEE TRANSACTIONS ON AUTOMATION SCIENCE AND ENGINEERING, 2024, 页码: 12
作者:  
An, Jiaxin;  Cao, Liang;  Wang, Yingxun;  Jadoon, Ahmer Khan;  Wang, Shuhui
  |  收藏  |  浏览/下载:6/0  |  提交时间:2024/12/06
Comparison of the Two Most Common Phenology Algorithms Imbedded in Land Surface Models 期刊论文  OAI收割
JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES, 2022, 卷号: 127, 期号: 21, 页码: 19
作者:  
Chen, Baozhang
  |  收藏  |  浏览/下载:27/0  |  提交时间:2023/01/30
Comparison of the Two Most Common Phenology Algorithms Imbedded in Land Surface Models 期刊论文  OAI收割
JOURNAL OF GEOPHYSICAL RESEARCH-ATMOSPHERES, 2022, 卷号: 127, 期号: 21, 页码: 19
作者:  
Chen, Baozhang
  |  收藏  |  浏览/下载:36/0  |  提交时间:2023/01/30
华北平原冬小麦——夏玉米轮作区DLM与CLM5模型模拟对比研究 CNKI期刊论文  OAI收割
2022
作者:  
王菲;  陈报章;  陈婧;  张慧芳;  郭立峰
  |  收藏  |  浏览/下载:34/0  |  提交时间:2022/09/30
Interaction of Th(IV) with graphene oxides: Batch experiments, XPS investigation, and modeling 期刊论文  OAI收割
JOURNAL OF MOLECULAR LIQUIDS, 2016, 卷号: 213, 期号: 无, 页码: 58-68
作者:  
Xu, Huan;  Li, Guang;  Li, Jie;  Chen, Changlun;  Ren, Xuemei
收藏  |  浏览/下载:21/0  |  提交时间:2017/07/24
陆面过程模型(DLM)关键结构与参数误差评估 学位论文  OAI收割
中国科学院地理科学与资源研究所: 中国科学院地理科学与资源研究所, 2015
作者:  
陈婧
  |  收藏  |  浏览/下载:24/0  |  提交时间:2023/07/05
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.  
东西方面孔识别机制的事件相关电位研究 学位论文  OAI收割
博士, 北京: 中国科学院研究生院, 2002
作者:  
彭小虎
收藏  |  浏览/下载:19/0  |  提交时间:2017/08/25