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Orbit and tracking data evaluation of Chang'E-4 relay satellite 期刊论文
ADVANCES IN SPACE RESEARCH, 2019, 卷号: 64, 期号: 4, 页码: 836-846
Authors:  Qin Songhe;  Huang Yong;  Li Peijia;  Shan Quan;  Fan Min;  Hu Xiaogong;  Wang Guangli
Favorite  |  View/Download:11/0  |  Submit date:2019/09/26
CE-4 relay satellite  Orbit determination  L2 point of Earth-Moon system  
A study on radio-loud interacting/non-interacting CMEs-associated SEPs and solar flares 期刊论文
ADVANCES IN SPACE RESEARCH, 2019, 卷号: 63, 期号: 10, 页码: 3390-3403
Authors:  Kalaivani, P. Pappa;  Prakash, O.;  Feng, Li;  Shanmugaraju, A.;  Ding, Liu-Guan;  Lu, Lei;  Gan, Weiqun
Favorite  |  View/Download:9/0  |  Submit date:2019/06/20
Solar energetic particle events (SEPs)  Radio-loud coronal mass ejections  Solar flares  m-to-DH type II radio bursts  
A combination method using evolutionary algorithms in initial orbit determination for too short arc 期刊论文
ADVANCES IN SPACE RESEARCH, 2019, 卷号: 63, 期号: 2, 页码: 999-1006
Authors:  Li, Xin-Ran;  Wang, Xin;  Xiong, Yong-qing
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Too short arc  Initial orbit determination  Estimation of distribution algorithm  Differential evolution  Evolutionary algorithm  
On the lunar node resonance of the orbital plane evolution of the Earth's satellite orbits 期刊论文
ADVANCES IN SPACE RESEARCH, 2018, 卷号: 61, 期号: 11, 页码: 2761-2776
Authors:  Zhu, Ting-Lei
Favorite  |  View/Download:3/0  |  Submit date:2019/04/08
Lunar node resonance  Medium Earth Orbit  Circular orbit  
An estimation of Envisat's rotational state accounting for the precession of its rotational axis caused by gravity-gradient torque 期刊论文
ADVANCES IN SPACE RESEARCH, 2018, 卷号: 61, 期号: 1, 页码: 182-188
Authors:  Lin, Hou-Yuan;  Zhao, Chang-Yin
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Envisat  Gravity-gradient torque  Rotational state estimation  Space debris  
Interferometry imaging technique for accurate deep-space probe positioning 期刊论文
ADVANCES IN SPACE RESEARCH, 2017, 卷号: 60, 期号: 12, 页码: 2847-2854
Authors:  Zheng, Weimin;  Tong, Fengxian;  Zhang, Juan;  Liu, Lei;  Shu, Fengchun
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Interferometry imaging  Accurate positioning  Lunar probe  MEX  VLBI  CVN  
The secular analytical solution of the orbital plane using Lindstedt-Poincare method 期刊论文
ADVANCES IN SPACE RESEARCH, 2017, 卷号: 60, 期号: 10, 页码: 2166-2180
Authors:  Yu, Shengxian;  Zhao, Changyin;  Zhang, Wei
Favorite  |  View/Download:3/0  |  Submit date:2019/04/08
Analytical solution  Space object  Lindstedt-Poincare procedure  
The fast co-adding algorithm of QCT 期刊论文
ADVANCES IN SPACE RESEARCH, 2017, 卷号: 60, 期号: 5, 页码: 907-914
Authors:  Ping, Yiding;  Zhang, Chen
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Image-processing  Instrumentation  Space debris  
Investigations of associated multi-band observations for GEO space debris 期刊论文
ADVANCES IN SPACE RESEARCH, 2017, 卷号: 59, 期号: 10, 页码: 2501-2511
Authors:  Lu, Yao;  Zhang, Chen;  Sun, Rong-yu;  Zhao, Chang-yin;  Xiong, Jian-ning
Adobe PDF(2498Kb)  |  Favorite  |  View/Download:11/0  |  Submit date:2019/04/08
Space debris  Geostationary orbit  Multi-band observations  Photometry  Light curves  
Long-term dynamical evolution of Tundra-type orbits 期刊论文
ADVANCES IN SPACE RESEARCH, 2017, 卷号: 59, 期号: 2, 页码: 682-697
Authors:  Zhang, Ming-Jiang;  Zhao, Chang-Yin;  Hou, Yong-Gang;  Zhu, Ting-Lei;  Wang, Hong-Bo;  Sun, Rong-Yu;  Zhang, Wei
Adobe PDF(2928Kb)  |  Favorite  |  View/Download:12/0  |  Submit date:2019/04/08
Tundra-type orbit  Dynamical evolution  1:1 tesseral resonance  Lunisolar perturbation