Three-axis Stabilization
Three-Axis Stabilization is a spacecraft attitude control method that maintains precise orientation along the roll, pitch, and yaw axes simultaneously by employing feedback control systems and onboard actuators to suppress angular deviations relative to a desired inertial or orbital reference frame.
105
Publications
3.6K
Citations
451
Authors
137
Institutions
Publications per year
2017–2026
24
Variants
Three-axis Attitude Control
Parents
105
1–5 of 105
451
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137

Beihang University
Beijing, China
10 h-index
28 publications
791 citations

Harbin Institute of Technology
Harbin, China
9 h-index
23 publications
907 citations

University of Surrey
Guildford, United Kingdom
4 h-index
8 publications
365 citations

Beijing Institute of Technology
Beijing, China
3 h-index
10 publications
210 citations

Sapienza University of Rome
Rome, Italy
3 h-index
4 publications
117 citations
Embry–Riddle Aeronautical University
Daytona, United States
3 h-index
6 publications
160 citations

Naval Postgraduate School
Monterey, United States
3 h-index
6 publications
177 citations
Massachusetts Institute of Technology
Cambridge, United States
3 h-index
11 publications
1.8K citations
1–8 of 137
10 publications · 468 citations
10
h-index
7 publications · 259 citations
7
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AST · 5 publications · 107 citations
4
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CJA · 3 publications · 65 citations
3
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2 publications · 30 citations
2
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1–5