中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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Assessment of the H2O2 budget at an urban site concerning the HO2 underprediction and the vertical transport from residual layers 期刊论文  OAI收割
ATMOSPHERIC ENVIRONMENT, 2022, 卷号: 272, 期号: 0, 页码: 118952
作者:  
Guo, Jia;  Wang, Zhe;  Cui, Yaru;  Zhang, Xiaoshan
  |  收藏  |  浏览/下载:17/0  |  提交时间:2022/11/07
Protective Geopolymer Coatings Containing Multi-Componential Precursors: Preparation and Basic Properties Characterization 期刊论文  OAI收割
MATERIALS, 2020, 卷号: 13, 期号: 16
作者:  
Jiang, Chenhui;  Wang, Aiying;  Bao, Xufan;  Chen, Zefeng;  Ni, Tongyuan
  |  收藏  |  浏览/下载:115/0  |  提交时间:2020/12/16
Whole-Brain Mapping of the Inputs and Outputs of the Medial Part of the Olfactory Tubercle 期刊论文  OAI收割
FRONTIERS IN NEURAL CIRCUITS, 2017, 卷号: 11
作者:  
Zhu, Xutao;  Liu, Qing;  Wang, Jie;  He, Xiaobin;  Wang, Huadong
  |  收藏  |  浏览/下载:41/0  |  提交时间:2017/12/06
Whole-Brain Mapping of the Inputs and Outputs of the Medial Part of the Olfactory Tubercle 期刊论文  OAI收割
FRONTIERS IN NEURAL CIRCUITS, 2017, 卷号: 11, 页码: 13
作者:  
Liu, Qing;  He, Xiaobin;  Wang, Jie;  Wang, Huadong;  Xu, Fuqiang
  |  收藏  |  浏览/下载:41/0  |  提交时间:2018/12/29
Space- and ground-based CO2 measurements: A review SCI/SSCI论文  OAI收割
2016
作者:  
Yue T. X.;  Zhang, L. L.;  Zhao, M. W.;  Wang, Y. F.;  Wilson, J.
收藏  |  浏览/下载:53/0  |  提交时间:2016/12/16
Toughening of amorphous poly(propylene carbonate) by rubbery CO2-based polyurethane: transition from brittle to ductile 期刊论文  OAI收割
rsc advances, 2015, 卷号: 5, 期号: 62, 页码: 49979-49986
作者:  
Ren,Guanjie;  Miao,Yuyang;  Qiao,Lijun;  Qin,Yusheng;  Wang,Xianhong
收藏  |  浏览/下载:96/0  |  提交时间:2016/05/20
Assessment of MODIS, MERIS, GEOV1 FPAR Products over Northern China with Ground Measured Data and by Analyzing Residential Effect in Mixed Pixel SCI/SSCI论文  OAI收割
2014
作者:  
Yang F.
收藏  |  浏览/下载:33/0  |  提交时间:2014/12/24
Toughening of poly(propylene carbonate) using rubbery non-isocyanate polyurethane: Transition from brittle to marginally tough 期刊论文  OAI收割
polymer, 2014, 卷号: 55, 期号: 21, 页码: 5460-5468
Ren, Guanjie; Sheng, Xingfeng; Qin, Yusheng; Chen,Xuesi; Wang,Xianhong; Wang,Fosong
收藏  |  浏览/下载:60/0  |  提交时间:2015/10/20
A shape context based Hausdorff similarity measure in image matching 会议论文  OAI收割
5th International Symposium on Photoelectronic Detection and Imaging (ISPDI) - Infrared Imaging and Applications, Beijing, June 25-27, 2013
作者:  
Ma TL(马天磊);  Liu YP(刘云鹏);  Shi ZL(史泽林);  Yin J(尹健)
收藏  |  浏览/下载:36/0  |  提交时间:2013/12/26
The traditional Hausdorff measure, which uses Euclidean distance metric (L2 norm) to define the distance between coordinates of any two points, has poor performance in the presence of the rotation and scale change although it is robust to the noise and occlusion. To address the problem, we define a novel similarity function including two parts in this paper. The first part is Hausdorff distance between shapes which is calculated by exploiting shape context that is rotation and scale invariant as the distance metric. The second part is the cost of matching between centroids. Unlike the traditional method, we use the centroid as reference point to obtain its shape context that embodies global information of the shape. Experiment results demonstrate that the function value between shapes is rotation and scale invariant and the matching accuracy of our algorithm is higher than that of previously proposed algorithm on the MEPG-7 database.  
The aircraft autopilot design of parameters changing in a wide range (EI CONFERENCE) 会议论文  OAI收割
2011 International Conference on Electric Information and Control Engineering, ICEICE 2011, April 15, 2011 - April 17, 2011, Wuhan, China
Zhen D.; Yue Z.
收藏  |  浏览/下载:28/0  |  提交时间:2013/03/25
Autopilot is an important part of aircraft  Under the action of the disturbance torque  for the flight parameters of aircraft Changing in a wide range  the range was about 16km  on the basic of analyzing the typical trajectory  the max height was about 5100m  the trajectory of feature points were selected  the deviation of lateral was about 12m  taking pitch control loop for example  the maximum angle of attack was about 3.6  a sub- PID autopilot was designed using classical control theory  the maximum elevator deflection was less than 5  using single-mode Transient suppression method  the maximum aileron deflection was less than 2  the overload due to control surface transition deflection was avoided when control parameters changing  the maximum roll was less than 5  the verification was done by non-linear simulation. The result showed that: the phase margin of autopilot was greater than 30  the response of overload can accurately track the given overload instruction. An autopilot design method of aircraft of parameter changes in a wide range was provided. 2011 IEEE.  the bandwidth was more than 14rad / s  the settling time was less than 0.7s  the maximum overshoot was 23.3%