Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Shengyong Tang"'
Publikováno v:
Journal of Guidance, Control, and Dynamics. 46:1219-1227
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::725393d969b6a04f43dc041bd2d06a45
https://doi.org/10.2514/1.g007198
https://doi.org/10.2514/1.g007198
Publikováno v:
AIAA Journal. 60:2718-2729
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::755811f183b617427ebf9ddd58c6681d
https://doi.org/10.2514/1.j060982
https://doi.org/10.2514/1.j060982
Autor:
Gang Wan, GuoBin Yu, ShengYong Tang, Wei Zeng, JiZhong Liu, XiaoJin Zhao, ChuanFei Zhang, WeiRen Wu, CangLi Liu, FuChuan Pang, AnWen Zhu, ShouLun Dai, WeiPing Liu, Qi Luo
Publikováno v:
SCIENTIA SINICA Technologica. 49:1-12
Space nuclear reactor power is the application of self-sustaining nuclear fission energy in space, which can fundamentally solve the bottleneck problem of high power demand of spacecraft in the future. It is also the premise of large-scale developmen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2a0ecfc968f4e378398626ae95b5f7e
https://doi.org/10.1360/n092018-00374
https://doi.org/10.1360/n092018-00374
Publikováno v:
Aerospace Science and Technology. 106:106075
In this paper, an innovative derivatives-based method is proposed to derive any higher-order integral-form Gauss's Variational Equations (GVEs) of the orbital elements under impulsive control. In this new method, the Taylor series expansion is applie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::41af55dae58700d531f5a66034d282af
https://doi.org/10.1016/j.ast.2020.106075
https://doi.org/10.1016/j.ast.2020.106075
Publikováno v:
2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC).
In this paper, the original nonlinear relative motion problem for a pair of satellites in which the leader is in a circular orbit is studied with a new perspective. This problem is regarded as a degenerate form of the circular restricted three-body p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::05d66e762cf033f4daaadcd1d3bc0c5a
https://doi.org/10.1109/cgncc.2016.7829177
https://doi.org/10.1109/cgncc.2016.7829177
Publikováno v:
Acta Astronautica. 75:136-153
Inner-Formation Gravity Measurement Satellite System (IFGMSS) is used to explore the Earth gravity using two satellites in an inner-formation flying mode. To fulfill the mission, relative position of the two satellites is required to be zeroed and at
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04a774a307e106c2275a0314731cac5c
https://doi.org/10.1016/j.actaastro.2012.02.006
https://doi.org/10.1016/j.actaastro.2012.02.006
Publikováno v:
Chinese Journal of Aeronautics. 24(3):299-308
Control allocation considers the problem of controlling instruction distribution for control systems with multiple and redundant actuators. This paper focuses on the direct allocation method, making the time requirement of the algorithm analogous com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fa064c7a553bec2a5206d894162e9c2d
Publikováno v:
Proceedings of the 31st Chinese Control Conference; 1/ 1/2012, p4334-4338, 5p
Publikováno v:
Proceedings of the 31st Chinese Control Conference; 1/ 1/2012, p4664-4669, 6p