Spacecraft Trajectory Optimization is a computational framework within trajectory optimization that specifically addresses the determination of optimal paths and control profiles for spacecraft under dynamic, gravitational, and operational constraints unique to space environments.
1K
Publications
39.3K
Citations
1.7K
Authors
422
Institutions
Publications per year
2017–2026
328
Parents
Publications
1K
Optimal trajectories for space navigation
D. G. King‐Hele · Planetary and Space Science · 1964 · 520 citations
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Authors
1.7K
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16
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- BABruce A. Conway
University of Illinois Urbana-Champaign, United States
16 publications · 1.7K citations
15
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- AA
14
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- GM
14
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- YL
13
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1–5 of 1.7K
Institutions
422
University of Illinois Urbana-Champaign
Urbana, United States
25 h-index
79 publications
5.7K citations
Jet Propulsion Laboratory
Pasadena, United States
25 h-index
86 publications
5.9K citations
Beijing Institute of Technology
Beijing, China
21 h-index
74 publications
2.8K citations
California Institute of Technology
Pasadena, United States
20 h-index
43 publications
2.8K citations
Harbin Institute of Technology
Harbin, China
20 h-index
119 publications
3.3K citations
Tsinghua University
Beijing, China
20 h-index
71 publications
2.1K citations
Massachusetts Institute of Technology
Cambridge, United States
20 h-index
47 publications
5.8K citations
National University of Defense Technology
Changsha, China
20 h-index
95 publications
3.1K citations
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Venues
- Journal of Guidance Control and Dynamics
203 publications · 12.5K citations
57
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- Journal of Spacecraft and Rockets
86 publications · 3.3K citations
32
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- Acta Astronautica
84 publications · 2.5K citations
30
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- Aerospace Science and Technology
AST · 56 publications · 1.7K citations
27
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- Advances in Space Research
37 publications · 1.1K citations
21
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