Control Derivatives
Control Derivatives is a stability and control analysis construct in aerospace engineering that quantifies the rate of change of aerodynamic forces and moments with respect to control surface deflections, distinguishing it from other stability derivatives by its exclusive dependence on actuated control inputs rather than vehicle state variables.
166
Publications
6K
Citations
336
Authors
129
Institutions
Publications per year
2017–2026
27
Parents
166
1–5 of 166
336
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129

Langley Research Center
Hampton, United States
15 h-index
32 publications
815 citations

Armstrong Flight Research Center
Edwards, United States
15 h-index
26 publications
834 citations

Ames Research Center
Mountain View, United States
10 h-index
14 publications
1.3K citations
University of Kansas
Lawrence, United States
6 h-index
18 publications
312 citations

Beihang University
Beijing, China
5 h-index
15 publications
465 citations
West Virginia University
Morgantown, United States
4 h-index
17 publications
279 citations

U.S. Air Force Institute of Technology
Dayton, United States
4 h-index
4 publications
283 citations
Systems Control (United States)
Iron Mountain, United States
4 h-index
8 publications
184 citations
1–8 of 129
15 publications · 520 citations
13
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Repository · 13 publications · 399 citations
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14 publications · 846 citations
12
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Conference · 7 publications · 221 citations
7
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Repository · 6 publications · 97 citations
6
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1–5