Lambert Problem Applications is a methodological framework in orbital mechanics that enables the determination of optimal transfer trajectories between celestial bodies by solving boundary-value problems for prescribed departure and arrival times, specifically leveraging solutions to Lambert's problem to support gravity-assist maneuver planning.
16
Publications
669
Citations
32
Authors
16
Institutions
Publications per year
2017–2026
4
Parents
Publications
16
1–5 of 16
Authors
32
- RP
3
h-index
- RW
1
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- KH
1
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- YL
1
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- ZW
1
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1–5 of 32
Institutions
16
The University of Texas at Austin
Austin, United States
3 h-index
6 publications
100 citations
University of the Basque Country
Leioa, Spain
1 h-index
3 publications
66 citations
Basque Center for Applied Mathematics
Bilbao, Spain
1 h-index
2 publications
44 citations
Space Information Laboratories (United States)
Santa Maria, United States
1 h-index
1 publications
17 citations
Iowa State University
Ames, United States
1 h-index
2 publications
26 citations
National University of Defense Technology
Changsha, China
1 h-index
4 publications
208 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
1 h-index
1 publications
14 citations
Texas A&M University
College Station, United States
1 h-index
5 publications
50 citations
1–8 of 16
Venues
- Journal of Guidance Control and Dynamics
6 publications · 256 citations
6
h-index
- Celestial Mechanics and Dynamical Astronomy
2 publications · 38 citations
2
h-index
- The Journal of the Astronautical Sciences
1 publications · 10 citations
1
h-index
- Canadian Journal of Physics
1 publications · 252 citations
1
h-index
- Advanced Maui Optical and Space Surveillance Technologies Conference
Conference · 1 publications · 11 citations
1
h-index
1–5