Lateral Coupled Dynamics
Lateral Coupled Dynamics is a dynamic stability phenomenon in aerospace engineering that characterizes the interaction between lateral and directional motions of an aircraft, wherein asymmetric rolling and yawing movements are inherently coupled due to aerodynamic and inertial cross-coupling effects.
23
Publications
549
Citations
66
Authors
29
Institutions
Publications per year
2017–2026
6
Parents
23
1–5 of 23
66
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29

Southwest Jiaotong University
Chengdu, China
3 h-index
11 publications
335 citations

University of Bristol
Bristol, United Kingdom
2 h-index
6 publications
174 citations
Politecnico di Milano
Milan, Italy
2 h-index
8 publications
145 citations

Tel Aviv University
Tel Aviv, Israel
1 h-index
3 publications
30 citations
Aeronautical Development Agency
Bengaluru, India
1 h-index
1 publications
28 citations
Cabot (United States)
Boston, United States
1 h-index
1 publications
13 citations
Purdue University West Lafayette
West Lafayette, United States
1 h-index
2 publications
24 citations

Northeastern University
Shenyang, China
1 h-index
1 publications
48 citations
1–8 of 29
5 publications · 111 citations
5
h-index
4 publications · 121 citations
4
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2 publications · 59 citations
2
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1 publications · 10 citations
1
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1 publications · 12 citations
1
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1–5