Orbit Perturbation Analysis
Orbit Perturbation Analysis is a systematic method within satellite geodesy that identifies, quantifies, and models deviations in a spacecraft's trajectory caused by non-gravitational and gravitational external forces, with particular emphasis on Solar Radiation Pressure effects, to refine orbital predictions and improve geodetic accuracy.
53
Publications
1.5K
Citations
131
Authors
62
Institutions
Publications per year
2017–2026
3
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62

European Space Operations Centre
Darmstadt, Germany
2 h-index
2 publications
77 citations
Jet Propulsion Laboratory
Pasadena, United States
2 h-index
5 publications
208 citations
In-Q-Tel
Arlington, United States
2 h-index
5 publications
185 citations

University of Rome Tor Vergata
Rome, Italy
2 h-index
5 publications
59 citations

Delft University of Technology
Delft, The Netherlands
2 h-index
5 publications
184 citations
The Aerospace Corporation
El Segundo, United States
2 h-index
4 publications
58 citations
National Institute for Astrophysics
Rome, Italy
2 h-index
2 publications
59 citations
Henan University of Science and Technology
Luoyang, China
1 h-index
2 publications
122 citations
1–8 of 62
8 publications · 304 citations
8
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4 publications · 108 citations
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3 publications · 60 citations
3
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AJ · 3 publications · 172 citations
3
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ApJ · 3 publications · 114 citations
3
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1–5