Reaction Wheel Control
Reaction Wheel Control is a spacecraft attitude control method that uses the angular momentum of a spinning flywheel to generate torque for precise orientation adjustments by varying the wheel's rotational speed in response to control commands.
255
Publications
7.7K
Citations
685
Authors
223
Institutions
Publications per year
2017–2026
55
Variants
Reaction Wheel Attitude Control
Parents
255
1–5 of 255
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223

Harbin Institute of Technology
Harbin, China
12 h-index
28 publications
989 citations
University of Michigan
Ann Arbor, United States
10 h-index
27 publications
916 citations
Jet Propulsion Laboratory
Pasadena, United States
10 h-index
53 publications
861 citations

University of Surrey
Guildford, United Kingdom
9 h-index
19 publications
763 citations
University of Colorado Boulder
Boulder, United States
8 h-index
14 publications
311 citations
California Institute of Technology
Pasadena, United States
6 h-index
20 publications
410 citations

Concordia University
Montreal, Canada
6 h-index
9 publications
338 citations
Massachusetts Institute of Technology
Cambridge, United States
5 h-index
15 publications
822 citations
1–8 of 223
38 publications · 1.5K citations
22
h-index
16 publications · 428 citations
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Conference · 7 publications · 91 citations
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6 publications · 137 citations
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Conference · 6 publications · 210 citations
6
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