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	Interferometry imaging technique for accurate deep-space probe positioning 期刊论文 OAI收割 ADVANCES IN SPACE RESEARCH, 2017, 卷号: 60, 期号: 12, 页码: 2847-2854 作者: Zheng, Weimin; Tong, Fengxian; Zhang, Juan; Liu, Lei; Shu, Fengchun \| 收藏 \| 浏览/下载：40/0 \| 提交时间：2019/04/08 Interferometry imaging Accurate positioning Lunar probe MEX VLBI CVN
	Interferometry imaging technique for accurate deep-space probe positioning 期刊论文 OAI收割 ADVANCES IN SPACE RESEARCH, 2017, 卷号: 60, 期号: 12, 页码: 2847-2854 作者: Zheng, Weimin; Tong, Fengxian; Zhang, Juan; Liu, Lei; Shu, Fengchun \| 收藏 \| 浏览/下载：43/0 \| 提交时间：2019/05/23 Interferometry Imaging Accurate Positioning Lunar Probe Mex Vlbi Cvn
	A method to estimate the neutral atmospheric density near the ionospheric main peak of Mars 期刊论文 OAI收割 JOURNAL OF GEOPHYSICAL RESEARCH-SPACE PHYSICS, 2016, 卷号: 121, 期号: 4, 页码: 3464-3475 作者: Zou, Hong; Ye, Yu Guang; Wang, Jin Song; Nielsen, Erling; Cui, Jun 收藏 \| 浏览/下载：26/0 \| 提交时间：2016/10/27 The neutral densities at 130 km can be derived fromtheMGS/RS measurements with our method The derived neutral densities can be used to verify or calibrate the Martian atmospheric model The method can be applied to other radio occultation measurements such as MEX/RS measurements
	Mars Express tracking and orbit determination trials with Chinese VLBI network 期刊论文 OAI收割 CHINESE SCIENCE BULLETIN, 2010, 卷号: 55, 期号: 32, 页码: 3654-3660 作者: Cao JianFeng; Huang Yong; Hu XiaoGong; Ma MaoLi; Zheng WeiMin 收藏 \| 浏览/下载：75/3 \| 提交时间：2011/06/29 VLBI MEX orbit determination
	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：25/0 \| 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.
	Semi-physical simulation of an optoelectronic tracking servo system based on C MEX S functions (EI CONFERENCE) 会议论文 OAI收割 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China Juan C.; Junhong Z. 收藏 \| 浏览/下载：24/0 \| 提交时间：2013/03/25 To the design of an optoelectronic tracking servo system we test the method [1 not only the reasonability of the control algorithm should be considered 2]. The simulation results verify the theoretical analysis. Because C MEX S function has the features of fast execute speed but the cost and time as well. It is necessary to establish the simulation model for the system. Applying the C MEX S functions independently generated program we can build the every independent digital control modules in MATLAB/SIMULINK for the optoelectronic tracking servo system. In the paper directly download to the hardwires we apply the C MEX S function to the design of the practical optoelectronic tracking servo system. For the speed we can design and debug the digital control modules in MATLAB/SIMULINK and then transform and download directly to DSP processor. 2010 IEEE. position loop control and TV delay compensations
	天然水体重金属迁移转化模型研究及其在乐安河水质研究中的应用学位论文 OAI收割硕士, 北京: 中国科学院研究生院, 1992 邹国强收藏 \| 浏览/下载：52/0 \| 提交时间：2011/09/19 重金属 NEW—MEX 模型乐安河