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IssuesArchive of Issues2023-7pp.2586-2594

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S.A. Kumakshev and A.M. Shmatkov, "Constraints in the Problem of Finding Optimal Trajectories for a Supersonic Non-Maneuverable Aircraft," Mech. Solids. 58 (7), 2586-2594 (2023)
Year 2023 Volume 58 Number 7 Pages 2586-2594
DOI 10.3103/S0025654423070130
Title Constraints in the Problem of Finding Optimal Trajectories for a Supersonic Non-Maneuverable Aircraft
Author(s) S.A. Kumakshev (Ishlinsky Institute for Problems in Mechanics of the Russian Academy of Sciences (IPMech RAS), Moscow, Russia, kumak@ipmnet.ru)
A.M. Shmatkov
Abstract 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 that must be satisfied by the flight altitude, pitch angle, normal overload, aircraft speed, engine thrust, etc., it is shown that almost all of these conditions can be ignored during the initial stage of calculations, since these constraints do not affect the optimal solutions. Therefore, one can first apply the maximum principle and use the dynamic programming method only in those cases where a sizeable part of the constraints turns out to be significant.
Keywords supersonic aircraft, optimal trajectory, phase constraint, dynamic programming method, maximum principle
Received 14 February 2023Revised 13 June 2023Accepted 20 June 2023
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