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	Alleviating the resolution limit problem in spatial community detection: a local network structure-based method 期刊论文 OAI收割 INTERNATIONAL JOURNAL OF GEOGRAPHICAL INFORMATION SCIENCE, 2025, 卷号: 39, 期号: 3, 页码: 510-532 作者: Liu, Wenkai; Cai, Haonan; Xing, Hanfa; Hu, Sheng; Tan, Zhangzhi \| 收藏 \| 浏览/下载：14/0 \| 提交时间：2025/03/18 Spatially embedded networks spatial community modularity function spatially constrained Leiden resolution limit problem
	Mining Hot Research Topics based on Complex Network Analysis - A Case Study on Regenerative Medicine 会议论文 OAI收割 the 9th International Joint Conference on Knowledge Discovery, Knowledge Engineering and Knowledge Management, 葡萄牙丰沙尔, 2017.11.1-2017.11.3 作者: Ceng RQ(曾荣强); Pang HS(庞弘燊); Tan XC(覃筱楚); Song YB(宋亦兵); Wen Y(文奕) 收藏 \| 浏览/下载：43/0 \| 提交时间：2017/12/17 Hot Research Topics Modularity Function Regenerative Medicine Community Detection Hypervolume Indicator
	Modular aircraft simulation platform based on simulink (EI CONFERENCE) 会议论文 OAI收割 2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China Chen C.-Q.; Ji Y. 收藏 \| 浏览/下载：26/0 \| 提交时间：2013/03/25 Aircraft simulation platform is the most important supporting technology in the aircraft development process. This simulation platform can be used for validating the design of subsystem and also it provides the necessary data for the Aircraft design. Wind has great impact on the flight parameter. In order to accurately simulate the wind model and calculate the flight parameters a simulation modeling method for flight parameter simulation platform under wind field environment is established. Firstly the various sub-systems which affecting flight parameters are analyzed some mathematical models of the flight parameter simulation platform is established. Secondly the atmospheric wind field is studied to analyze the impact on its trajectory. Then the model is built in the Simulink toolbox in the Matlab which is based on the principles of hierarchy and modularity using C MEX S-function for the complex kinetic equations. Finally when the models have been established encapsulating models for several subsystem and assembling them for the Aircraft simulation platform based on the unified interface. The simulation tests (including the performance test of a certain gliding Aircraft the wind influence test of a certain uncontrolled aircraft) prove the simulation capability of the platform and its calculating step can reach 1 ms. Comparing simulation with field test data of a certain uncontrolled aircraft it shows that the relative deviation of range is 0.47% the relative deviation of maximal altitude is 2.1%. Taking relevant standards as a reference standard it is demonstrated the platform is reliable meets the engineering accuracy requirements. 2010 IEEE.