Flight Path Angle Dynamics
Flight Path Angle Dynamics is a mathematical model in longitudinal flight dynamics that characterizes the time-varying behavior of the angle between the aircraft's velocity vector and the local horizontal plane, distinguishing itself by its focus on the trajectory倾角's evolution during climb, cruise, and descent phases under aerodynamic, propulsive, and gravitational forces.
72
Publications
3K
Citations
167
Authors
72
Institutions
Publications per year
2017–2026
14
Parents
72
1–5 of 72
167
United States Air Force Research Laboratory, United States
5 publications · 822 citations
5
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5
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5
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4
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4
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1–5 of 167
72

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
7 h-index
12 publications
1.7K citations

Beihang University
Beijing, China
6 h-index
17 publications
420 citations
Georgia Institute of Technology
Atlanta, United States
5 h-index
9 publications
229 citations
The Ohio State University
Columbus, United States
4 h-index
8 publications
1.5K citations

Ames Research Center
Mountain View, United States
4 h-index
5 publications
168 citations
Agency for Defense Development
Daejeon, South Korea
4 h-index
8 publications
369 citations
Korea Advanced Institute of Science and Technology
Daejeon, South Korea
4 h-index
4 publications
167 citations
Wichita State University
Wichita, United States
3 h-index
10 publications
160 citations
1–8 of 72
14 publications · 1.1K citations
11
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Conference · 4 publications · 161 citations
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4 publications · 89 citations
4
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3 publications · 123 citations
3
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3 publications · 244 citations
3
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1–5