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长春光学精密机械与... [10]
光电技术研究所 [1]
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会议论文 [10]
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Atmospheric carbon dioxide profile detection with a continuous-wave differential absorption lidar
期刊论文
OAI收割
OPTICS AND LASERS IN ENGINEERING, 2024, 卷号: 180
作者:
Hua, Zhenzhen
;
Huang, Jian
;
Shi, Dongfeng
;
Yuan, Kee
;
Hu, Shunxing
  |  
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2024/11/20
Differential absorption lidar (DIAL)
Carbon dioxide (CO 2 )
Scheimpflug imaging principle
Identification of geo-bodies in borehole radar image based on Curvelet transform
期刊论文
OAI收割
JOURNAL OF APPLIED GEOPHYSICS, 2021, 卷号: 189, 页码: 9
作者:
Li, Li
;
Wang, Rui
;
Peng, Tianxiang
;
Hao, Jingyi
;
Zhou, Zhipeng
  |  
收藏
  |  
浏览/下载:42/0
  |  
提交时间:2021/06/18
Ground Penetrating Radar
Imaging principle of GPR
Curvelet transform
Reflected energy
Identification of geo-bodies
The analyze and design of focusing system for space camera (EI CONFERENCE)
会议论文
OAI收割
2012 International Conference on Electrical Insulating Materials and Electrical Engineering, EIMEE 2012, May 25, 2012 - May 27, 2012, Shenyang, Liaoning, China
作者:
Yu T.
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2013/03/25
In order to control the focal plane and guarantee the imaging quality of space camera
the focusing system was proposed. Firstly
the reasons of defocusing were analyzed and a solution method was given. Secondly
the system structure and operating principle were introduced. Thirdly
the system design was presented in detail. Finally
the system was experimented. Experimental results indicate that the defocusing amount of camera can be controlled below 10 um and the focusing system satisfies the requirement of system design. (2012) Trans Tech Publications
Switzerland.
The research on statistical properties of TDI-CCD imaging noise (EI CONFERENCE)
会议论文
OAI收割
International Symposium on Photoelectronic Detection and Imaging 2011: Advances in Imaging Detectors and Applications, May 24, 2011 - May 26, 2011, Beijing, China
Gu Y.-Y.
;
Shen X.-H.
;
He G.-X.
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2013/03/25
TDI-CCD can improve the sensitivity of space camera without any degradation of spatial resolution which is widely used in aerospace imaging devices. The article describes the basic working principle and application characteristics of TDI-CCD devices
analyses the composition of TDI-CCD imaging noise
and propose a new method to analyze TDI-CCD imaging noise with statistical probability distribution. In order to estimate the distribution of gray values affect by noise we introduced the concept of skewness and kurtosis. We design an experiment using constant illumination light source
take image with TDI-CCD working at different stage such as stage 16
stage 32
stage 48
stage 64 and stage 96
analyse the characteristics of image noise with the method we proposed
experimental results show that the gray values approximately meet normal distribution in large sample cases. 2011 SPIE.
Study on spectrograph for ionosphere: A broadband imaging instrument prototype for far-ultraviolet (EI CONFERENCE)
会议论文
OAI收割
International Symposium on Photoelectronic Detection and Imaging 2011: Space Exploration Technologies and Applications, May 24, 2011 - May 26, 2011, Beijing, China
作者:
Wang S.-R.
收藏
  |  
浏览/下载:36/0
  |  
提交时间:2013/03/25
Current research on space-based exploration for the ionosphere needs more advanced technologies. Because the spectral signals in the ionosphere distributing basically in the far-ultraviolet waveband are very weak. Usual spectrometer structures and detectors such as CCD can't receive enough information. Based on this principle of atmospheric sounding
the imaging spectrometer prototype for ionosphere detection application was designed to solve the problem. This prototype consists of the telescope and the imaging spectrometer. The simple structure and small number of mirrors can help higher transmission efficiency be achieved and weak signals detection be implemented. The telescope is an off-axis parabolic mirror and the spectrometer is a modified Czerny-Turner spectral imaging system. Modified Czerny-Turner spectrometer contains a spherical mirror
a fixed plane grating and a toroidal mirror. By adjusting the incident angle to the collimating mirror and using toroidal mirror
coma and astigmatism were corrected well. We also optimize distances between the grating to the focusing mirror and the focusing mirror to the image plane to improve disadvantages of traditional Czerny-Turner structure. Designed results demonstrate that aberrations are substantially corrected
and high image quality can be obtained in broad waveband. The photon counting Wedge-Strip-Anode detector with micro-channel planes as the receiving plane is accepted for the instrument prototype. The other photon counting 2-D detector responding well for weak light such as Cross-Delay line detector and MAMA detector can also be used for detection. The calibration and performances testing system is made of a vacuum system
a deuterium lamp
a monochrometer and the instrument prototype. Results obtained from the experiment show that the spectral resolution is 2.4 nm and the spatial resolution is 80 m. The other calibration experiments are running. The technology of the spectrometer prototype is important for the research and applications of ionosphere remote sensing. 2011 SPIE.
Design of motion compensation mechanism of satellite remote sensing camera (EI CONFERENCE)
会议论文
OAI收割
International Symposium on Photoelectronic Detection and Imaging 2011: Space Exploration Technologies and Applications, May 24, 2011 - May 26, 2011, Beijing, China
Gu S.
;
Yan Y.
;
Xu K.
;
Jin G.
收藏
  |  
浏览/下载:47/0
  |  
提交时间:2013/03/25
With the development of aerospace remote sensing technology
the ground resolution of remote sensing camera enhances continuously. Since there is relative motion between camera and ground target when taking pictures
the target image recorded in recording media is moved and blurred. In order to enhance the imaging quality and resolution of the camera
the image motion had to be compensated. In order to abate the effect of image motion to image quality of space camera and improve the resolution of the camera
the compensation method of image motion to space camera is researched. First
the reason of producing drift angle and adjustment principle are analyzed in this paper. This paper introduce the composition and transmission principle of image motion compensation mechanism. Second
the system adopts 80C31 as controller of drift angle
and adopts stepping motor for actuators
and adopts absolute photoelectric encoder as the drift Angle measuring element. Then the control mathematical model of the image motion compensation mechanism are deduced
and it achieve the closed-loop control of the drift angle position. At the last
this paper analyses the transmission precision of the mechanism. Through the experiment
we measured the actual precision of the image motion compensation mechanism
and compared with the theoretical analysis. There are two major contributions in this paper. First
the traditional image motion compensation mechanism is big volume and quality heavy. This has not fit for the development trend of space camera miniaturization and lightweight. But if reduce the volume and quality of mechanism
it will bring adverse effects for the precision and stiffness of mechanism. For this problem
This paper designed a image motion compensation that have some advantages such as small size
light weight at the same time
high precision
stiffness and so on. This image motion compensation can be applicable to the small optics cameras with high resolution. Second
the traditional mechanism control need to corrected
fitting and iterative for the control formula of mechanism. Only in this way
we can get the optimal control mathematical model. This paper has high precision of the control formula derived. It can achieve the high precision control without fitting
It also simplify the difficulty of control mathematical model establishment. This paper designed the range of adjusting of image motion compensation mechanism between -5 +5. Based on choosing-5
-4
-3
-2
-1
0
+1
+2
+3
+4
+4 as the expectation value of the imaginary drift angle
we get ten groups of the fact data in adjusting drift angle measured. The test results show that the precision of the drift angle control system can be achieved in 1. It can meet the system requirements that the precision of the control system is less than 3'
and it can achieve the high-precision image motion compensation. 2011 SPIE.
Study on the flutter model of the imaging quality of TDICCD space camera (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Advanced Engineering Materials and Technology, AEMT 2011, July 29, 2011 - July 31, 2011, Sanya, China
作者:
Chen X.
;
Chen X.
;
Chen X.
收藏
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浏览/下载:28/0
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提交时间:2013/03/25
For any On-orbit Space camera
the influence of flutter on the imaging process of TDICCD space camera is inevitable
thus causing the decline of image quality. This paper briefly introduces the principle of TIDCCD camera and how flutter affects the imaging process. Then through the analysis and calculation of practical program
we find the acceleration criterion to avoid the blur of image quality. (2011) Trans Tech Publications.
Image forward motion compensation method for some aerial reconnaissance camera based on neural network predictive control (EI CONFERENCE)
会议论文
OAI收割
International Conference on Advanced Research on Computer Science and Information Engineering, CSIE 2011, May 21, 2011 - May 22, 2011, Zhengzhou, China
Zhong C.
;
Ding Y.
;
Fu J.
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2013/03/25
In this paper
neural network predictive control method is used to compensate the image forward motion of a certain aerial reconnaissance camera and we have solved several problems that traditional control methods have. Firstly
according to the principle of imaging
we analyzed the reasons for the existence of image forward motion and established the mathematical model. Secondly
we analyzed the theoretically feasibility of the method. At last
simulation
experiments and test are used to validate the practical feasibility. Through what we have done
we conclude that neural network predictive control method can be used to compensate image forward motion for this certain camera and can make a perfect performance. 2011 Springer-Verlag.
Design and analysis of auto-focus assembly for spaceborne remote sensing camera (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electronics, Communications and Control, ICECC 2011, September 9, 2011 - September 11, 2011, Ningbo, China
作者:
Chen W.
;
Gao X.
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2013/03/25
Spaceborne remote sensing camera may be out of focus when the environment and photographic distance changes. In order to get higher ground sampled distance for the camera
based on the experience gained from the development of a remote sensing camera
working principle of auto-focus assembly control system was discussed. Time of waveform extraction was reduced. It sets force an auto-focus assembly that uses cam and line guide rail in order to move the lens group. The motion error of the auto-focus assembly was difficult to be eliminated and would affect on the focusing accuracy of the spaceborne remote sensing camera directly. So it was analyzed at both ends of the focusing structure. The CCD detector can keep stable when the remote sensing camera is imaging. The motion error was tested to verify the validity of the simulation result and it is less than 0.01mm. Its accuracy meets using demand. The focusing method of moving focal plane is suitable for spaceborne remote sensing camera. 2011 IEEE.
Image motion compensation for a certain aviation camera based on Lucy-Richardson algorithm (EI CONFERENCE)
会议论文
OAI收割
2011 International Conference on Electronics and Optoelectronics, ICEOE 2011, July 29, 2011 - July 31, 2011, Dalian, China
Zhong C.
;
Fu J.
;
Ding Y.
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2013/03/25
According to the actual situation
when high quality and high precision are required for the image
both beforehand and afterwards compensation should be used. In this paper
we use Lucy-Richardson algorithm to compensate image motion of a certain aviation camera as an afterwards compensation. Firstly
we analyze the imaging principle of the camera and the reasons that cause image motion. Then we have a brief introduce of the Lucy-Richardson algorithm. At last
in order to show the feasibility of the method
we do some simulation. Through theoretical and practical analysis
experiments and test
we conclude the Lucy-Richardson algorithm can be used to compensate image motion for the certain camera. 2011 IEEE.