Transfer Orbit Design
Transfer Orbit Design is a methodological framework within spacecraft trajectory design that specifically governs the formulation and optimization of orbital transfer paths, distinguished by its focus on determining the most efficient trajectory parameters, timing, and maneuver sequences to transition a spacecraft between initial and target orbits while satisfying mission constraints.
12
Publications
284
Citations
30
Authors
15
Institutions
Publications per year
2017–2026
2
12
1–5 of 12
30
1
h-index
1
h-index
1
h-index
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h-index
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h-index
1–5 of 30
15
Jet Propulsion Laboratory
Pasadena, United States
3 h-index
5 publications
127 citations
China Astronaut Research and Training Center
Beijing, China
1 h-index
1 publications
33 citations
Vikram Sarabhai Space Centre
Thiruvananthapuram, India
1 h-index
2 publications
28 citations

National University of Defense Technology
Changsha, China
1 h-index
2 publications
66 citations
Beijing Aerospace Flight Control Center
Beijing, China
1 h-index
1 publications
10 citations
Purdue University West Lafayette
West Lafayette, United States
1 h-index
2 publications
98 citations
Korea Advanced Institute of Science and Technology
Daejeon, South Korea
1 h-index
2 publications
40 citations
Goddard Space Flight Center
Greenbelt, United States
1 h-index
2 publications
46 citations
1–8 of 15
2 publications · 46 citations
2
h-index
1 publications · 49 citations
1
h-index
1 publications · 33 citations
1
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1 publications · 28 citations
1
h-index
1 publications · 11 citations
1
h-index
1–5