中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
首页
机构
成果
学者
登录
注册
登陆
×
验证码:
换一张
忘记密码?
记住我
×
校外用户登录
CAS IR Grid
机构
长春光学精密机械与物... [4]
重庆绿色智能技术研究... [1]
合肥物质科学研究院 [1]
采集方式
OAI收割 [6]
内容类型
会议论文 [3]
期刊论文 [3]
发表日期
2024 [1]
2018 [1]
2016 [1]
2011 [1]
2010 [1]
2006 [1]
更多
学科主题
筛选
浏览/检索结果:
共6条,第1-6条
帮助
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
提交时间升序
提交时间降序
作者升序
作者降序
题名升序
题名降序
发表日期升序
发表日期降序
An improved LIO-SAM algorithm by integrating image information for dynamic and unstructured environments
期刊论文
OAI收割
MEASUREMENT SCIENCE AND TECHNOLOGY, 2024, 卷号: 35
作者:
Meng, Xinyu
;
Chen, Xi
;
Chen, Shaofeng
;
Fang, Yongfeng
;
Fan, Hao
  |  
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2024/11/20
object-aware simultaneous localization and mapping (SLAM)
dynamic scenes
JPDA data association
velocity integration
Image Motion Velocity Model and Compensation Strategy of Wide-Field Remote Sensing Camera
期刊论文
OAI收割
Wuhan Daxue Xuebao (Xinxi Kexue Ban)/Geomatics and Information Science of Wuhan University, 2018, 卷号: 43, 期号: 8, 页码: 1278-1286
作者:
Li, Yongchang
;
Jin, Longxu
;
Li, Guoning
;
Wu, Yinan
;
Wang, Wenhua
  |  
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2019/09/17
Remote sensing
Cameras
Global optimization
Image quality
Integration
Mirrors
Motion compensation
Orbits
Satellites
Velocity
Influence of filtration velocity on DON variation in BAF for micropolluted surface water treatment
期刊论文
OAI收割
ENVIRONMENTAL SCIENCE AND POLLUTION RESEARCH, 2016, 卷号: 23, 期号: 23, 页码: 23415-23421
作者:
Ma, Teng-Fei
;
Chen, You-Peng
;
Kang, Jia
;
Gao, Xu
;
Guo, Jin-Song
  |  
收藏
  |  
浏览/下载:189/0
  |  
提交时间:2018/03/15
Dissolved organic nitrogen
Micropolluted surface water
Biological aerated filter
Filtration velocity
3D excitation-emission matrix fluorescence spectroscopy
Fluorescence regional integration technique
Geocentric distance's errors' correction of space cameras based on USGS DEM (EI CONFERENCE)
会议论文
OAI收割
2011 IEEE 3rd International Conference on Communication Software and Networks, ICCSN 2011, May 27, 2011 - May 29, 2011, Xi'an, China
作者:
Li W.
;
Li W.
;
Xu S.
收藏
  |  
浏览/下载:37/0
  |  
提交时间:2013/03/25
In order to correct the geocentric distance's error of TDI (Time Delay and Integration) CCD space camera in calculation of image motion compensation
the data source of the earth's height above sea level USGS DEM (United States Geological Survey Digital Elevation Model) has been introduced to make digital elevation map
the match error of the forward direction (the integral direction of TDI CCD) has been greatly decreased by correcting the geocentric distance error
and eliminate the influence to the relative error of image motion velocity
and correct the error generated by the different heights above sea level. After correcting
which greatly improves the imaging quality of TDI CCD space camera. 2011 IEEE.
a model of image motion calculation of nadir has been introduced
the calculation and analysis of the model shows that: the maximum error of image motion velocity about 1.72% has been decreased to 0.06%
and the influence of the geocentric distance error to the relative error of image motion velocity has been analyzed with the model
Design of ground-based physical simulation system for satellite-borne TDI-CCD dynamic imaging (EI CONFERENCE)
会议论文
OAI收割
Optoelectronic Imaging and Multimedia Technology, October 18, 2010 - October 20, 2010, Beijing, China
作者:
Zhang L.
;
Zhang L.
;
Sun Z.
收藏
  |  
浏览/下载:33/0
  |  
提交时间:2013/03/25
As we know
the existence of image motion has a bad effect on the image quality of satellite-borne TDI CCD camera. Although many theories on image motion are proposed to cope with this problem
few simulations are done to justify the proposed theories on ground. And thus
in this paper
a ground-based physical simulation system for TDI CCD imaging is developed and specified
which consists of a physical simulation subsystem for precise satellite attitude control based on a 3-axis air bearing table
and an imaging and simulation subsystem utilizing area-array CCD to simulate TDI CCD. The designed system could realize not only a precise simulation of satellite attitude control
whose point accuracy is above 0.1 and steady accuracy above 0.01/s
but also an imaging simulation of 16-stage TDI CCD with 0.1s its integration time. This paper also gives a mathematical model of image motion of this system analogous with satellite-borne TDI CCD
and detailed descriptions on the principle utilizing area-array CCD to simulate TDI CCD. It is shown that experiment results are in accordance with mathematical simulation
and that the image quality deteriorate seriously when the correspondence between the image velocity and signal charges transfer velocity is broken out
which suggest not only the validity of the system design but also the validity of the proposed image motion theory of TDI CCD. 2010 SPIE.
Design of GPS/INS integrated navigation system based on multisensor information fusion (EI CONFERENCE)
会议论文
OAI收割
6th World Congress on Intelligent Control and Automation, WCICA 2006, June 21, 2006 - June 23, 2006, Dalian, China
Chunmei H.
;
Yantao T.
;
Wanxin S.
;
Mao L.
收藏
  |  
浏览/下载:51/0
  |  
提交时间:2013/03/25
Two kinds of design methods of GPS/INS integrated navigation system are presented
that is GPS/INS integrative system and integrated navigation system based on information fusion. By analyzing mathematics model of the first system error
we found that inertia velocity error would cause code loop track error. Consequently
the pseudo range meterage error is interrelated with inertia velocity error
which is complex to calculate. If this relativity is ignored in the state equation and observation equation of this system
it must affect the estimated precision of the kalman filter and maybe the system is unstable. Therefore
the second integrated navigation method is introduced. It adopts information fusion
federal kalman filter and covariance. And consider the above pertinence to analyze the navigation performance of the integration system. Then it gives the flow of federal kalman filter algorithm. By analyzing
the conclusion is that velocity error of integrated navigation system drops from 0.5m/s to below 0.05m/s
and improves the precision and reliability of the navigation system effectively
well continuity and real-time capability. It provides an effective way for data analysis and process of fusion navigation system. 2006 IEEE.