Control Surface Actuation
Control Surface Actuation is a mechanical or electromechanical process by which pilot commands or automated flight control system outputs are translated into physical movement of aircraft control surfaces through the operation of actuators that directly apply force to those surfaces.
24
Publications
738
Citations
69
Authors
32
Institutions
Publications per year
2017–2026
2
Parents
24
1–5 of 24
69
3
h-index
2
h-index
2
h-index
2
h-index
2
h-index
1–5 of 69
32
Systems Technology (United States)
Hawthorne, United States
3 h-index
4 publications
125 citations
Auburn University
Auburn, United States
2 h-index
3 publications
79 citations
Georgia Institute of Technology
Atlanta, United States
2 h-index
6 publications
162 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
2 h-index
2 publications
85 citations
Northrop Grumman (United States)
Falls Church, United States
2 h-index
5 publications
182 citations
Hoh Aeronautics (United States)
Lomita, United States
2 h-index
2 publications
75 citations

École Nationale Supérieure de Mécanique et d'Aérotechnique
Chasseneuil-du-Poitou, France
1 h-index
2 publications
158 citations
Virginia Tech
Blacksburg, United States
1 h-index
2 publications
94 citations
1–8 of 32
4 publications · 221 citations
4
h-index
2 publications · 53 citations
2
h-index
Conference · 1 publications · 29 citations
1
h-index
Conference · 1 publications · 32 citations
1
h-index
SMS · 1 publications · 29 citations
1
h-index
1–5