Orbital Maneuvers
Orbital Maneuvers is a fundamental concept in astrodynamics and orbital mechanics denoting the controlled changes in a spacecraft's trajectory or orbital elements through the application of propulsive forces to achieve specific mission objectives.
2K
Publications
77K
Citations
3.8K
Authors
835
Institutions
Publications per year
2017–2026
495
2K
SPACECRAFT ATTITUDE DETERMINATION AND CONTROL
J. B. Wertz · 1978 · 1.3K citations
Orbital mechanics for engineering students
Choice Reviews Online · 2005 · 613 citations
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835

Harbin Institute of Technology
Harbin, China
37 h-index
233 publications
9.2K citations
Tsinghua University
Beijing, China
28 h-index
166 publications
5.1K citations

Beihang University
Beijing, China
27 h-index
122 publications
4.8K citations

National University of Defense Technology
Changsha, China
26 h-index
175 publications
5K citations
Jet Propulsion Laboratory
Pasadena, United States
26 h-index
131 publications
7.8K citations

Northwestern Polytechnical University
Xi'an, China
25 h-index
120 publications
5.2K citations

Beijing Institute of Technology
Beijing, China
24 h-index
112 publications
3.7K citations
University of Colorado Boulder
Boulder, United States
22 h-index
93 publications
2.8K citations
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390 publications · 19.5K citations
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275 publications · 8.2K citations
45
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AST · 101 publications · 4.3K citations
39
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128 publications · 3.5K citations
31
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98 publications · 2.9K citations
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