Control Coupling
Control Coupling is a static aeroelastic phenomenon in aircraft stability wherein the deformation of the airframe under aerodynamic loads induces unintended changes in control surface effectiveness or aircraft response, thereby coupling otherwise independent control inputs to rigid-body motions.
67
Publications
3K
Citations
175
Authors
80
Institutions
Publications per year
2017–2026
28
67
Tight Formation Flight Control
Meir Pachter, J. D'Azzo, Andrew Proud · Journal of Guidance Control and Dynamics · 2001 · 262 citations
1–5 of 67
175
7
h-index
5
h-index
2
h-index
2
h-index
2
h-index
1–5 of 175
80

Nankai University
Tianjin, China
8 h-index
24 publications
1.5K citations

City University of Hong Kong
Hong Kong, Hong Kong
3 h-index
7 publications
386 citations

Huazhong University of Science and Technology
Wuhan, China
3 h-index
10 publications
174 citations
École Polytechnique Fédérale de Lausanne
Lausanne, Switzerland
2 h-index
1 publications
45 citations
Beijing Jiaotong University
Beijing, China
2 h-index
4 publications
128 citations

Zhejiang University of Technology
Hangzhou, China
2 h-index
5 publications
130 citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
2 h-index
2 publications
44 citations
China University of Mining and Technology
Xuzhou, China
2 h-index
4 publications
65 citations
1–8 of 80
4 publications · 366 citations
4
h-index
4 publications · 283 citations
4
h-index
2 publications · 171 citations
2
h-index
2 publications · 52 citations
2
h-index
2 publications · 82 citations
2
h-index
1–5