Orbital Transfer Optimization is a trajectory optimization problem that specifically involves determining the most efficient spacecraft transfer path between two orbits by minimizing a performance index such as fuel consumption or transfer time while satisfying orbital dynamics and mission constraints.
104
Publications
3.3K
Citations
189
Authors
90
Institutions
Publications per year
2017–2026
19
Parents
Publications
104
1–5 of 104
Authors
189
- AM
9
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- VK
4
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- AE
3
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3
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1–5 of 189
Institutions
90
Rice University
Houston, United States
9 h-index
20 publications
482 citations
The Aerospace Corporation
El Segundo, United States
6 h-index
8 publications
278 citations
Northwestern Polytechnical University
Xi'an, China
3 h-index
6 publications
114 citations
Iowa State University
Ames, United States
3 h-index
5 publications
319 citations
Jet Propulsion Laboratory
Pasadena, United States
3 h-index
5 publications
71 citations
Glenn Research Center
Cleveland, United States
3 h-index
4 publications
49 citations
University of Illinois Urbana-Champaign
Urbana, United States
3 h-index
4 publications
604 citations
Georgia Institute of Technology
Atlanta, United States
3 h-index
4 publications
157 citations
1–8 of 90
Venues
- Journal of Guidance Control and Dynamics
20 publications · 1.1K citations
17
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- Acta Astronautica
13 publications · 419 citations
12
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- AIAA Journal
6 publications · 178 citations
6
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- Aerospace Science and Technology
AST · 6 publications · 107 citations
6
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- The Journal of the Astronautical Sciences
6 publications · 184 citations
6
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