Integrated Propulsion Control
Integrated Propulsion Control is a control framework that unifies propulsion system management with aircraft flight control laws to optimize overall vehicle performance, stability, and responsiveness during dynamic maneuvers by enabling coordinated, real-time adjustments between thrust generation and aerodynamic control effectors.
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1.2K
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62
Authors
28
Institutions
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2017–2026
2
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Sylvain Martel, Mahmood Mohammadi, Ouajdi Felfoul et al. · The International Journal of Robotics Research · 2009 · 453 citations · Full text
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Glenn Research Center
Cleveland, United States
6 h-index
7 publications
182 citations

University of Leicester
Leicester, United Kingdom
5 h-index
13 publications
244 citations

Armstrong Flight Research Center
Edwards, United States
3 h-index
6 publications
81 citations
James S. McDonnell Foundation
St Louis, United States
2 h-index
4 publications
72 citations
Northrop Grumman (United States)
Falls Church, United States
2 h-index
6 publications
72 citations
Stanford University
Stanford, United States
2 h-index
4 publications
46 citations
Edwards Air Force Base
Edwards Air Force Base, United States
2 h-index
2 publications
36 citations

Ames Research Center
Mountain View, United States
2 h-index
4 publications
146 citations
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5 publications · 79 citations
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3 publications · 50 citations
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Conference · 2 publications · 52 citations
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2 publications · 47 citations
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AST · 1 publications · 35 citations
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