Linearized Missile Models
Linearized Missile Models is a mathematical modeling approach in missile flight dynamics that approximates the nonlinear equations of motion through linearization about a steady-state operating point, enabling tractable stability and control analysis using linear system theory.
56
Publications
2K
Citations
115
Authors
49
Institutions
Publications per year
2017–2026
6
Parents
56
1–5 of 56
115
6
h-index
4
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3
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United States Air Force Research Laboratory, United States
2 publications · 196 citations
2
h-index
1–5 of 115
49
Technion – Israel Institute of Technology
Haifa, Israel
10 h-index
20 publications
866 citations
United States Air Force
Arlington, United States
3 h-index
6 publications
447 citations
Louisiana State University
Baton Rouge, United States
2 h-index
4 publications
106 citations
Optimal Synthesis (United States)
Los Altos, United States
2 h-index
5 publications
200 citations

Northwestern Polytechnical University
Xi'an, China
2 h-index
5 publications
97 citations

Eglin Air Force Base
Eglin Air Force Base, United States
2 h-index
3 publications
87 citations

Naval Surface Warfare Center
Washington, United States
2 h-index
4 publications
116 citations

U.S. Air Force Institute of Technology
Dayton, United States
2 h-index
4 publications
436 citations
1–8 of 49
15 publications · 769 citations
14
h-index
Conference · 2 publications · 61 citations
2
h-index
Conference · 2 publications · 39 citations
2
h-index
2 publications · 93 citations
2
h-index
2 publications · 36 citations
2
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1–5