Maneuver Trim
Maneuver Trim is a flight control system state within the broader category of trim conditions, distinguished by its specific equilibrium configuration during accelerated flight maneuvers, wherein aerodynamic, propulsive, and inertial forces and moments are balanced to maintain a desired non-steady, non-level flight path.
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2017–2026
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Masato Nakamura, Takeshi Imamura, Nobuaki Ishii et al. · Earth Planets and Space · 2016 · 124 citations · Full text
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National Institute of Advanced Industrial Science and Technology, Japan
1 publications · 124 citations
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Technion – Israel Institute of Technology
Haifa, Israel
2 h-index
3 publications
89 citations
Hokkaido Information University
Ebetsu, Japan
1 h-index
1 publications
124 citations

Kobe University
Kobe, Japan
1 h-index
1 publications
124 citations

Tokyo Gakugei University
Tokyo, Japan
1 h-index
2 publications
248 citations
Rikkyo University
Tokyo, Japan
1 h-index
1 publications
124 citations

University of Padua
Padua, Italy
1 h-index
3 publications
54 citations

National Institute of Information and Communications Technology
Tokyo, Japan
1 h-index
1 publications
124 citations
University of Shiga Prefecture
Hikone, Japan
1 h-index
1 publications
124 citations
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2 publications · 89 citations
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1 publications · 18 citations
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1 publications · 63 citations
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1 publications · 29 citations
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1 publications · 124 citations
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