Integrated Flight Control Design
Integrated Flight Control Design is a multidisciplinary optimization framework that systematically unifies aerodynamic, structural, and control system models within the aeroelastic design process to simultaneously enhance aircraft performance, stability, and maneuverability through synergistic interaction of flight control laws and elastic airframe behavior.
47
Publications
1.5K
Citations
145
Authors
49
Institutions
Publications per year
2017–2026
9
Parents
47
1–5 of 47
145
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1–5 of 145
49

Glenn Research Center
Cleveland, United States
6 h-index
8 publications
189 citations

University of Leicester
Leicester, United Kingdom
4 h-index
10 publications
132 citations

Langley Research Center
Hampton, United States
3 h-index
3 publications
85 citations

University of Minnesota
Minneapolis, United States
2 h-index
5 publications
158 citations
University of Maryland, College Park
College Park, United States
2 h-index
7 publications
298 citations

Pennsylvania State University
State College, United States
2 h-index
3 publications
43 citations
Arizona State University
Tempe, United States
2 h-index
5 publications
116 citations

Boeing (United States)
Chicago, United States
2 h-index
4 publications
122 citations
1–8 of 49
4 publications · 183 citations
4
h-index
3 publications · 43 citations
3
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Conference · 2 publications · 72 citations
2
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Repository · 2 publications · 76 citations
2
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2 publications · 47 citations
2
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1–5