Constraints in the Problem of Finding Optimal Trajectories for a Supersonic Non-Maneuverable Aircraft

The influence of phase and other constraints on the method of searching for the trajectories of a civil supersonic aircraft that are optimal in terms of fuel consumption is considered. Based on the solutions found by the dynamic programming method, which take into account the numerous conditions tha...

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Vydané v:	Mechanics of solids Ročník 58; číslo 7; s. 2586 - 2594
Hlavní autori:	Kumakshev, S. A., Shmatkov, A. M.
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Moscow Pleiades Publishing 01.12.2023
Predmet:	Classical Mechanics Physics Physics and Astronomy optimal trajectory maximum principle dynamic programming method supersonic aircraft phase constraint
ISSN:	0025-6544, 1934-7936
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