Active Attitude Control
Active Attitude Control is a control methodology within the domain of spacecraft attitude dynamics that employs powered actuators and real-time feedback to deliberately alter and stabilize the orientation of a spacecraft, distinguishing it from passive or natural stabilization techniques by its reliance on continuous energy input and active intervention.
94
Publications
4K
Citations
250
Authors
107
Institutions
Publications per year
2017–2026
33
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250
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107

Beihang University
Beijing, China
10 h-index
32 publications
951 citations

Harbin Institute of Technology
Harbin, China
6 h-index
11 publications
856 citations

Sapienza University of Rome
Rome, Italy
3 h-index
6 publications
387 citations

University of L'Aquila
L’Aquila, Italy
3 h-index
7 publications
192 citations

Glenn Research Center
Cleveland, United States
3 h-index
5 publications
108 citations

Beijing Institute of Technology
Beijing, China
3 h-index
5 publications
218 citations
Jet Propulsion Laboratory
Pasadena, United States
3 h-index
6 publications
380 citations
University of California, Berkeley
Berkeley, United States
2 h-index
8 publications
370 citations
1–8 of 107
8 publications · 568 citations
8
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AST · 7 publications · 531 citations
7
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7 publications · 193 citations
7
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Repository · 3 publications · 41 citations
3
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3 publications · 52 citations
3
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1–5