Trim Equations is a mathematical framework consisting of a set of steady-state equilibrium equations that govern the balance of forces and moments acting on an aircraft, distinguishing it by its specific application to determining stable flight conditions in which all rotational and translational accelerations are zero.
8
Publications
262
Citations
14
Authors
10
Institutions
Publications per year
2017–2026
0
Parents
Publications
8
1–5 of 8
Authors
14
- BC
2
h-index
- MC
2
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- MK
1
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- BW
1
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- LB
1
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1–5 of 14
Institutions
10
Cranfield University
Cranfield, United Kingdom
2 h-index
2 publications
31 citations
University of Oklahoma
Norman, United States
2 h-index
2 publications
31 citations
Technion – Israel Institute of Technology
Haifa, Israel
1 h-index
2 publications
58 citations
IBM (Brazil)
São Paulo, Brazil
1 h-index
1 publications
116 citations
University of Maryland, College Park
College Park, United States
1 h-index
3 publications
72 citations
Langley Research Center
Hampton, United States
1 h-index
1 publications
19 citations
Pennsylvania State University
State College, United States
1 h-index
1 publications
19 citations
Honeywell (United States)
Charlotte, United States
1 h-index
2 publications
42 citations
1–8 of 10
Venues
- AIAA Atmospheric Flight Mechanics Conference and Exhibit
Conference · 2 publications · 31 citations
2
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- AIAA Journal
2 publications · 48 citations
2
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- Journal of Aircraft
1 publications · 24 citations
1
h-index
- Transportation Research Part E Logistics and Transportation Review
1 publications · 22 citations
1
h-index
- Journal of Guidance Control and Dynamics
1 publications · 21 citations
1
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1–5