Orbit Design
Orbit Design is a methodological framework within astrodynamics that specifies the construction and optimization of trajectories for spacecraft positioned at or near Lagrange points, distinguished by its integration of gravitational equilibrium conditions and orbital stability constraints inherent to the circular restricted three-body problem.
371
Publications
13.2K
Citations
1.2K
Authors
343
Institutions
Publications per year
2017–2026
80
Parents
371
The COSMIC/FORMOSAT-3 Mission: Early Results
Richard A. Anthes, P. A. Bernhardt, Y. Chen et al. · Bulletin of the American Meteorological Society · 2008 · 1.1K citations · Full text
1–5 of 371
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343
Jet Propulsion Laboratory
Pasadena, United States
20 h-index
100 publications
28.4K citations
Purdue University West Lafayette
West Lafayette, United States
13 h-index
36 publications
1.3K citations
Goddard Space Flight Center
Greenbelt, United States
13 h-index
69 publications
2.3K citations
California Institute of Technology
Pasadena, United States
11 h-index
21 publications
655 citations

University of Strathclyde
Glasgow, United Kingdom
11 h-index
23 publications
1.3K citations
Tsinghua University
Beijing, China
10 h-index
20 publications
643 citations
University of Colorado Boulder
Boulder, United States
10 h-index
15 publications
333 citations

National University of Defense Technology
Changsha, China
9 h-index
30 publications
612 citations
1–8 of 343
50 publications · 1.6K citations
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32 publications · 1.1K citations
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31 publications · 968 citations
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19 publications · 503 citations
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Repository · 13 publications · 296 citations
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