Sun-pointing Dynamics
Sun-Pointing Dynamics is a control-theoretic framework within attitude-orbit coupling that governs the orientation and orbital motion of a spacecraft to maintain a fixed alignment with the Sun, distinguished by its integration of solar vector referencing with coupled rotational and translational dynamics for precision pointing and orbit stabilization.
35
Publications
1.5K
Citations
109
Authors
39
Institutions
Publications per year
2017–2026
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University of Pisa
Pisa, Italy
3 h-index
9 publications
185 citations
Rockwell Automation (United States)
Milwaukee, United States
2 h-index
5 publications
74 citations
The University of Tokyo
Tokyo, Japan
2 h-index
3 publications
57 citations
University of California, Santa Barbara
Santa Barbara, United States
2 h-index
6 publications
76 citations

Universidad Politécnica de Madrid
Madrid, Spain
2 h-index
4 publications
63 citations
Tsinghua University
Beijing, China
2 h-index
5 publications
145 citations

University of Glasgow
Glasgow, United Kingdom
2 h-index
2 publications
53 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
2 h-index
19 publications
354 citations
1–8 of 39
5 publications · 445 citations
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4 publications · 149 citations
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3 publications · 68 citations
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2 publications · 314 citations
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Repository · 2 publications · 24 citations
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