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Retrieval of atmospheric mass densities in lower thermosphere below 200 km from precise orbit of re-entry object CZ-3B R/B by analytical and numerical methods 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2018, 卷号: 363, 期号: 8, 页码: 11
Authors:  Zhang, Ming-Jiang;  Wang, Hong-Bo;  Zhao, Chang-Yin;  Xiong, Jian-Ning;  Wei, Dong;  Zhang, Wei;  Yu, Sheng-Xian
Favorite  |  View/Download:7/0  |  Submit date:2019/04/08
Atmospheric mass density  Precise orbit  Re-entry object  Analytical method  Numerical method  
Analytic model for the long-term evolution of circular Earth satellite orbits including lunar node regression 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2017, 卷号: 362, 期号: 4, 页码: 9
Authors:  Zhu, Ting-Lei;  Zhao, Chang-Yin;  Zhang, Ming-Jiang
Adobe PDF(1077Kb)  |  Favorite  |  View/Download:8/0  |  Submit date:2019/04/08
Orbital plane evolution  Milankovitch element  Lunar node regression  Analytic approximation  
Variation ranges of motion parameters for space debris in the geosynchronous ring 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2016, 卷号: 361, 期号: 6
Authors:  Zhao, Chang-Yin;  Zhang, Ming-Jiang;  Yu, Sheng-Xian;  Xiong, Jian-Ning;  Zhang, Wei;  Zhu, Ting-Lei
Adobe PDF(1358Kb)  |  Favorite  |  View/Download:15/0  |  Submit date:2016/09/27
Space Debris  Geosynchronous Ring  Motion Parameter  Variation Range  
Control of tetrahedron satellite formation flying in the geosynchronous orbit using solar radiation pressure 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2016, 卷号: 361, 期号: 4
Authors:  Hou, Yong-Gang;  Zhang, Ming-Jiang;  Zhao, Chang-Yin;  Sun, Rong-Yu
Adobe PDF(1250Kb)  |  Favorite  |  View/Download:18/0  |  Submit date:2016/09/27
Celestial Mechanics  Tetrahedron Satellite Formation Flying  Control  Solar Radiation Pressure  
Analysis on the long term orbital evolution of Molniya satellites 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2015, 卷号: 357, 期号: 2, 页码: 126
Authors:  Zhu, Ting-Lei;  Zhao, Chang-Yin;  Wang, Hong-Bo;  Zhang, Ming-Jiang
Adobe PDF(2611Kb)  |  Favorite  |  View/Download:75/0  |  Submit date:2015/12/03
Semi-major Axis  Luni-solar Resonance  Resonance Overlap  Critical Inclination  Large Eccentricity  
Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2015, 卷号: 355, 期号: 2, 页码: 203-212
Authors:  Zhang, Ming-Jiang;  Zhao, Chang-Yin
Adobe PDF(476Kb)  |  Favorite  |  View/Download:78/0  |  Submit date:2015/12/03
Attitude Stability  Dual-spin Spacecraft  Asteroid  Conditions Of Stability  
Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2014, 卷号: 351, 期号: 2, 页码: 507-524
Authors:  Zhang, Ming-Jiang;  Zhao, Chang-Yin
Adobe PDF(1470Kb)  |  Favorite  |  View/Download:316/2  |  Submit date:2014/11/20
Spacecraft  Asteroid  Attitude Stability  Sufficient Conditions Of Stability  Stability Domain  
Reply to: "Comment on the paper 'On the triangular libration points in photogravitational restricted three-body problem with variable mass'" by Varvoglis, H. and Hadjidemetriou, J.D. 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2012, 卷号: 340, 期号: 2, 页码: 209-210
Authors:  Zhang, Ming-Jiang
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Variable Mass  Restricted Three-body Problem  
On the triangular libration points in photogravitational restricted three-body problem with variable mass 期刊论文
ASTROPHYSICS AND SPACE SCIENCE, 2012, 卷号: 337, 期号: 1, 页码: 107-113
Authors:  Zhang, Ming-Jiang;  Zhao, Chang-Yin;  Xiong, Yong-Qing
Adobe PDF(306Kb)  |  Favorite  |  View/Download:420/4  |  Submit date:2013/01/31
Celestial Mechanics  Variable Mass  Restricted Three-body Problem