Trajectory Correction Maneuvers
Trajectory Correction Maneuvers is a navigational procedure in astrodynamics consisting of controlled propulsive adjustments to a spacecraft's flight path, distinguished from other trajectory modifications by its purpose of correcting deviations from the intended interplanetary trajectory due to launch inaccuracies, gravitational perturbations, or other dispersions.
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Publications
598
Citations
113
Authors
37
Institutions
Publications per year
2017–2026
11
Variants
Tcms
Parents
28
Halo orbit mission correction maneuvers using optimal control
Radu Serban, Wang Sang Koon, Martin W. Lo et al. · Automatica · 2002 · 78 citations
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Jet Propulsion Laboratory
Pasadena, United States
6 h-index
22 publications
488 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
4 h-index
8 publications
167 citations
Institute of Space and Astronautical Science
Tokyo, Japan
3 h-index
6 publications
158 citations

Beihang University
Beijing, China
2 h-index
4 publications
80 citations
California Institute of Technology
Pasadena, United States
2 h-index
4 publications
248 citations
Wuhan University of Technology
Wuhan, China
1 h-index
4 publications
76 citations

Université Fédérale de Toulouse Midi-Pyrénées
Toulouse, France
1 h-index
3 publications
81 citations
Universitat de Barcelona
Barcelona, Spain
1 h-index
2 publications
44 citations
1–8 of 37
Conference · 3 publications · 45 citations
3
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3 publications · 60 citations
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3 publications · 63 citations
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Repository · 3 publications · 39 citations
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2 publications · 35 citations
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