Two-Aircraft optimal control problem. The in-flight noise reduction

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dc.contributor.authorNahayo, Fulgence
dc.contributor.authorKhardi, Salah
dc.contributor.authorHaddou,Mounir
dc.contributor.authorEt al.
dc.date.accessioned2025-01-09T08:57:14Z
dc.date.available2025-01-09T08:57:14Z
dc.date.issued2012
dc.descriptionArticle
dc.description.abstractThe aim of this paper is to present and solve a mathematical model of a two-aircraft optimal control problem reducing the noise on the ground during the approach. The mathematical modelization of this problem is a non-convex optimal control governed by ordinary non-linear differential equations. To solve this problem, A direct method and a Runge-Kutta RK4 discretization schema are used. This discretization schema is chosed because it is a sufficiently high order and it does-not require computation of the partial derivatives of the aircraft dynamic. The Nonlinear Interior point Trust Region Optimization solver KNITRO is applied. A large set of numerical experiments is presented. The obtained results give feasible trajectories with a significant noise reduction.
dc.identifier.urihttps://repository.ub.edu.bi/handle/123456789/1302
dc.publisherResearchGate
dc.titleTwo-Aircraft optimal control problem. The in-flight noise reduction
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