Perturbed Lambert Problem
The Perturbed Lambert Problem is a variant of the classical Lambert's Problem in orbital mechanics that incorporates perturbing forces—such as gravitational anomalies, atmospheric drag, or third-body effects—into the boundary value problem for determining spacecraft trajectories between two position vectors within a specified time of flight.
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A unified form of Lambert's theorem
Robert C. Blanchard, E. R. Lancaster · NASA Technical Reports Server (NASA) · 1968 · 56 citations · Full text
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The University of Texas at Austin
Austin, United States
5 h-index
9 publications
189 citations
Texas A&M University
College Station, United States
5 h-index
13 publications
281 citations

National University of Defense Technology
Changsha, China
3 h-index
11 publications
499 citations
Khalifa University of Science and Technology
Abu Dhabi, United Arab Emirates
2 h-index
2 publications
60 citations

Harbin Institute of Technology
Harbin, China
2 h-index
4 publications
94 citations
Institut de Mécanique Céleste et de Calcul des Éphémérides
Paris, France
1 h-index
1 publications
10 citations
Virginia Tech
Blacksburg, United States
1 h-index
2 publications
98 citations
PLA Rocket Force University of Engineering
Xi'an, China
1 h-index
1 publications
17 citations
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11 publications · 361 citations
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Repository · 1 publications · 56 citations
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