Analytical and simulation model of fighter flight dynamics with a limiter for the permissible flight envelope when performing the split-S maneuver

The article substantiates the relevance to develop an analytical-simulation model of fighter flight dynamics with a limiter for the permissible flight envelope during the split-S maneuver. The structure of the analytical and simulation model of a fighter, consisting of a combination of a flight test...

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Bibliographic Details
Main Authors: P. S. Kostin, K. A. Zhuravskiy
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2023-08-01
Series:Научный вестник МГТУ ГА
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/2224
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