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CAS IR Grid
机构
金属研究所 [10]
国家空间科学中心 [2]
长春光学精密机械与物... [2]
地质与地球物理研究所 [1]
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OAI收割 [16]
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期刊论文 [14]
会议论文 [2]
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2023 [1]
2019 [1]
2013 [2]
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空间物理 [1]
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Prediction of geosynchronous electron fluxes using an artificial neural network driven by solar wind parameters
期刊论文
OAI收割
ADVANCES IN SPACE RESEARCH, 2023, 卷号: 71, 期号: 1, 页码: 275-285
作者:
Wang, Jianhang
;
Guo, Deyu
;
Xiang, Zheng
;
Ni, Binbin
;
Liu, Yangxizi
  |  
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2023/03/30
Flux prediction
Artificial neural network
Geosynchronous orbit
Solar wind parameters
Contribution analysis of inter-satellite ranging observation to BDS-2 satellite orbit determination based on regional tracking stations
期刊论文
OAI收割
ACTA ASTRONAUTICA, 2019, 卷号: 164, 页码: 297-310
作者:
Zhang, Rui
;
Tu, Rui
;
Fan, Lihong
;
Zhang, Pengfei
;
Liu, Jinhai
  |  
收藏
  |  
浏览/下载:18/0
  |  
提交时间:2020/11/11
BDS satellite orbit determination
China regional ground tracking stations
Inter-satellite ranging observation
Contribution analysis
Dynamic parameters dilution of precision
Satellite position dilution of precision
Simulation of number and distribution of Compass occultation events
期刊论文
OAI收割
CHINESE JOURNAL OF GEOPHYSICS-CHINESE EDITION, 2013, 卷号: 56, 期号: 8, 页码: 2522-2530
作者:
Wang Xian-Yi
;
Sun Yue-Qiang
;
Bai Wei-Hua
;
Du Qi-Fei
;
Wang Dong-Wei
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2014/04/30
Compass navigation system
Low Earth Orbit
Occultation
Orbit parameters
Simulation
Theoretical studies of EPR parameters and defect structures for Ni2+ ions in corundum
期刊论文
OAI收割
Physica B-Condensed Matter, 2013, 卷号: 408, 页码: 169-174
W. Fang
;
Q. W. Wang
;
W. Y. Yang
;
W. C. Zheng
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2013/12/24
Fourth-order perturbation formulae
Two spin-orbit coupling parameter
Defect structure
[NiO6](10-) cluster
paramagnetic resonance absorption
spin-hamiltonian parameters
trigonal
crystal-field
centers
pressure
nickel
al2o3
3d(8)
Theoretical investigation of optical spectra and covalent effect of Cr4+ in Y2Ti2O7 and Y2Sn2O7
期刊论文
OAI收割
Physica B-Condensed Matter, 2012, 卷号: 407, 期号: 12, 页码: 2344-2346
W. L. Feng
;
J. Y. Xue
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2013/02/05
Optical spectra
Covalent effect
Two spin-orbit coupling parameters
model
Cr4+
Y2Ti2O7 and Y2Sn2O7
atomic screening constants
tetragonal distortion
scf functions
crystal
epr
pyrochlores
parameters
growth
sites
Design and calibration of the solar irradiance monitor (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:
Yang D.-J.
;
Gong C.-H.
;
Wang Y.-P.
;
Ye X.
;
Fang W.
收藏
  |  
浏览/下载:27/0
  |  
提交时间:2013/03/25
The solar irradiance monitor (SIM)
with the design accuracy of 5
used to monitor the secular changes of the total solar irradiance on FY-3 satellite
takes the sun-scanning measurement method on-orbit. Compared to the sun-tracking measurement method
this method simplifies the structure and cuts the cost
but the measuring accuracy is affected by the sun-synchronous orbit
sunlight incidence angle and the installing angle of the SIM in the satellite. Through the ground calibration experiment
studies on the affection of different sunlight incidence angles to the measurement accuracy. First
by the satellite tool kit (STK) simulation software
simulates the orbital parameters of the sun-synchronous satellite
and calculates the Sun ascension and declination at any time. By the orbit coordinate transformation matrix gets the components of the Sun vectors to the axes of the satellite
and base on the components designs the field of view and the installing angles of the SIM. Then
designs and completes the calibration experiment to calibrate the affection of the incidence angles. Selecting 11 different angles between the sunlight and the satellite X-axis
measures the total solar irradiance by the SIM at each angle
and compares to the irradiances of the SIAR reference radiometers
and gets the coefficient curves of the three channels of the SIM. Finally
by the quadratic fitting
gets the correction equations on the incidence angles: R 1=5.7110-52 -2.45310 -3+1.0302
R2=2.8410-5-1. 96510-3+1.0314 and R3 =1.7210 -52-4.18410-4+0.9946. The equations will aimprove the on-orbit measurement accuracy of the solar irradiance
and are very important to the on-orbit data processing after the satellite launched. 2011 SPIE.
Theoretical investigation for the EPR g-factors of the mixed ground state in NaCl: Ag(2+) crystals
期刊论文
OAI收割
Spectrochimica Acta Part a-Molecular and Biomolecular Spectroscopy, 2011, 卷号: 79, 期号: 5, 页码: 1308-1310
W. L. Li
;
X. M. Li
;
W. L. Feng
;
W. J. Yang
;
C. Y. Tao
收藏
  |  
浏览/下载:26/0
  |  
提交时间:2012/04/13
Electron paramagnetic resonance
Double spin-orbit coupling model
NaCl
Ag(2+)
spin-hamiltonian parameters
atomic screening constants
paramagnetic-resonance
single-crystals
optical-spectra
scf functions
ions
electrons
sites
v3+
Theoretical Explanations of the g Factors for Ni(3+) Ions in KMgF(3) and CsCaF(3) Crystals
期刊论文
OAI收割
Spectroscopy Letters, 2010, 卷号: 43, 期号: 1, 页码: 40912
L. He
;
W. C. Zheng
;
S. R. Zhang
收藏
  |  
浏览/下载:37/0
  |  
提交时间:2012/04/13
crystal- and ligand-field theory
CsCaF3
electron paramagnetic
resonance
KMgF3
Ni3+
spin transition
spin-hamiltonian parameters
atomic screening constants
other-orbit
interactions
electronic spectra
scf functions
field
mgo
transition
distortion
complexes
Study on the absorption spectra and electron paramagnetic resonance g factors of RbNiCl(3) single crystal
期刊论文
OAI收割
Physica B-Condensed Matter, 2010, 卷号: 405, 期号: 18, 页码: 3831-3833
W. L. Feng
;
X. M. Li
;
T. Li
;
L. C. Pu
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2012/04/13
Crystal- and ligand-field theory
Optical spectra
Electron paramagnetic
resonance (EPR)
Spin-orbit coupling
atomic screening constants
optical-spectra
scf functions
spin
parameters
field
epr
csnicl3
systems
chain
Analysis of laser jamming to satellite-based detector (EI CONFERENCE)
会议论文
OAI收割
International Symposium on Photoelectronic Detection and Imaging 2009: Laser Sensing and Imaging, June 17, 2009 - June 19, 2009, Beijing, China
作者:
Guo L.-H.
;
Guo R.-H.
;
Wang S.-W.
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2013/03/25
The reconnaissance satellite
communication satellite and navigation satellite used in the military applications have played more and more important role in the advanced technique wars and already become the significant support and aid system for military actions. With the development of all kinds of satellites
anti-satellite laser weapons emerge as the times require. The experiments and analyses of laser disturbing CCD (charge coupled detector) in near ground have been studied by many research groups
but their results are not suitable to the case that using laser disturbs the satellite-based detector. Because the distance between the satellite-based detector and the ground is very large
it is difficult to damage it directly. However the optical receive system of satellite detector has large optical gain
so laser disturbing satellite detector is possible. In order to determine its feasibility
the theoretical analyses and experimental study are carried out in the paper. Firstly
the influence factors of laser disturbing satellite detector are analyzed in detail
which including laser power density on the surface of the detector after long distance transmission
and laser power density threshold for disturbing etc. These factors are not only induced by the satellite orbit
but dependence on the following parameters: laser average power in the ground
laser beam quality
tracing and aiming precision and atmospheric transmission. A calculation model is developed by considering all factors which then the power density entering into the detector can be calculated. Secondly
the laser disturbing experiment is performed by using LD (laser diode) with the wavelength 808 nm disturbing CCD 5 kilometer away
which the disturbing threshold value is obtained as 3.5510-4mW/cm2 that coincides with other researcher's results. Finally
using the theoretical model
the energy density of laser on the photosensitive surface of MSTI-3 satellite detector is estimated as about 100mW/cm2
which is largely exceed the disturbing threshold and therefore verify the feasibility of using this kind of laser disturbing the satellite-based detector. According to the results. using the similar laser power density absolutely saturate the requirements to laser disturbing satellite-based detector. If considering the peak power of pulsed laser
even decrease laser average power
it is also possible to damage the detector. This result will provide the reliable evidences to evaluate the effect of laser disturbing satellite-based detector. 2009 SPIE.