Coordinated Turn Dynamics
Coordinated Turn Dynamics is a theoretical framework within lateral-directional flight dynamics that characterizes the coupled roll-yaw-pitch motion of an aircraft during a turn in which the lateral acceleration is minimized through balanced control inputs, thereby maintaining a zero sideslip condition.
30
Publications
1.1K
Citations
70
Authors
36
Institutions
Publications per year
2017–2026
5
30
1–5 of 30
70
4
h-index
4
h-index
2
h-index
2
h-index
2
h-index
1–5 of 70
36
University of Lisbon
Lisbon, Portugal
4 h-index
8 publications
462 citations
University of Maryland, College Park
College Park, United States
2 h-index
7 publications
188 citations
Defence Science and Technology Group
Canberra, Australia
2 h-index
2 publications
45 citations
Instituto Politécnico de Lisboa
Lisbon, Portugal
2 h-index
4 publications
366 citations

Linköping University
Linköping, Sweden
2 h-index
4 publications
230 citations

Xi'an Jiaotong University
Xi'an, China
2 h-index
8 publications
200 citations
Sierra Nevada Corporation (United States)
Sparks, United States
1 h-index
1 publications
70 citations
University of Southampton
Southampton, United Kingdom
1 h-index
1 publications
17 citations
1–8 of 36
3 publications · 199 citations
3
h-index
Conference · 1 publications · 17 citations
1
h-index
1 publications · 75 citations
1
h-index
1 publications · 76 citations
1
h-index
1 publications · 26 citations
1
h-index
1–5