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《交通运输系统工程与信息》 EI CSCD 2011年第6期216-221,共6页
关键词 JUN PAGE PING LI Author Index Page number refers to the first page of paper
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Subject Index Page number refers to the first page of paper
2
《交通运输系统工程与信息》 EI CSCD 2011年第6期206-215,共10页
关键词 PAGE Subject Index Page number refers to the first page of paper MODE
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Author Index Page number refers tothe first page of paper
3
《交通运输系统工程与信息》 EI CSCD 2009年第6期181-186,共6页
关键词 交通运输系统工程 PAGE PING Author Index Page number refers tothe first page of paper
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Subject Index Page number refers tothe first page of paper
4
《交通运输系统工程与信息》 EI CSCD 2009年第6期173-180,共8页
关键词 PAGE SIMULATION Subject Index Page number refers tothe first page of paper 交通运输系统工程
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Journal of Transportation Systems Engineering and Information Technology Author Index Page number refers tothe first page of paper
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《交通运输系统工程与信息》 EI CSCD 2006年第6期182-186,共5页
关键词 PING PAGE Journal of Transportation Systems Engineering and Information Technology Author Index Page number refers tothe first page of paper
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Journal of Transportation Systems Engineering and Information Technology Subject Index Page number refers tothe first page of paper
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《交通运输系统工程与信息》 EI CSCD 2006年第6期174-181,共8页
关键词 PAGE Journal of Transportation Systems Engineering and Information Technology Subject Index Page number refers tothe first page of paper MODE
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Reference satellite selection method for GNSS high-precision relative positioning
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作者 Xiao Gao Wujiao Dai +1 位作者 Zhiyong Song Changsheng Cai 《Geodesy and Geodynamics》 2017年第2期125-129,共5页
Selecting the optimal reference satellite is an important component of high-precision relat/ve positioning because the reference satellite directly influences the strength of the normal equation. The reference satelli... Selecting the optimal reference satellite is an important component of high-precision relat/ve positioning because the reference satellite directly influences the strength of the normal equation. The reference satellite selection methods based on elevation and positional dilution of precision (PDOP) value were compared. Results show that all the above methods cannot select the optimal reference satellite. We introduce condition number of the design matrix in the reference satellite selection method to improve structure of the normal equation, because condition number can indicate the ill condition of the normal equation. The experimental results show that the new method can improve positioning accuracy and reliability in precise relative positioning. 展开更多
关键词 Global Navigation Satellite System (GNSS)Relative positioning Reference satellite Positional dilution of precision (PDOP)Condition number
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Effects of rarefaction on the characteristics of micro gas journal bearings 被引量:8
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作者 Hai-jun ZHANG Chang-sheng ZHU Ming TANG 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2010年第1期43-49,共7页
Given the definition of the reference Knudsen number for micro gas journal bearings,the range in the number is related to the viscosity of air at different temperatures. A modified Reynolds equation for micro gas jour... Given the definition of the reference Knudsen number for micro gas journal bearings,the range in the number is related to the viscosity of air at different temperatures. A modified Reynolds equation for micro gas journal bearings based on Burgdorfer's first-order slip boundary condition is proposed that takes into account the gas rarefaction effect. The finite difference method (FDM) is adopted to solve the modified Reynolds equation to obtain the pressure profiles,load capacities and attitude angles for micro gas journal bearings at different reference Knudsen numbers,bearing numbers and journal eccentricity ratios. Numerical analysis shows that pressure profiles and non-dimensional load capacities decrease markedly as gas rarefaction in-creases. Attitude angles change conversely,and when the eccentricity ratio is less than 0.6,the attitude angles rise slightly and the influence of the reference Knudsen number is not marked. In addition,the effect of gas rarefaction on the non-dimensional load capacity and attitude angle decreases with smaller bearing numbers. 展开更多
关键词 Reference Knudsen number Rarefaction effect Reynolds equation Finite difference method (FDM)
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