Controlled deployment of a long tether to operate as a partial space elevator

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Astrodynamics Pub Date : 2024-06-10 DOI:10.1007/s42064-024-0225-5
Jinbang Huang, Arun K. Misra
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受控部署长系绳,作为部分太空电梯运行
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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
期刊最新文献
Initial orbit determination of some cislunar orbits based on short-arc optical observations Controlled deployment of a long tether to operate as a partial space elevator Real-time hybrid method for maneuver detection and estimation of non-cooperative space targets Message from the Guest Editors of the Special Issue on Tethered Satellite System Optimal orbit transfer of single-tether E-sail with inertially fixed spin axis
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