Optimal control of two-commercial aircraft dynamic system during approachReport as inadecuate




Optimal control of two-commercial aircraft dynamic system during approach - Download this document for free, or read online. Document in PDF available to download.

1 University of Burundi 2 INRETS-LTE - Laboratoire Transport et Environnement 3 MAPMO - Mathématiques - Analyse, Probabilités, Modélisation - Orléans

Abstract : This paper aims to reduce noise levels of two-aircraft landing simultaneously on approach. Constraints related to stability, performance and flight safety are taken into account. The problem of optimal control is described and solved by a Sequential Quadratic Programming numerical method -SQP- when globalized by the trust region method. By using a merit function, a sequential quadratic programming method associated with global trust regions bypasses the non-convex problem. This method used a nonlinear interior point trust region optimization solver under AMPL. Among several possible solutions, it is shown that there is an optimal trajectory leading to a reduction of noise levels on approach.

Mots-clés : AVION BRUIT TRAJECTOIRE OPTIMISATION





Author: Fulgence Nahayo - Salah Khardi - Mounir Haddou -

Source: https://hal.archives-ouvertes.fr/



DOWNLOAD PDF




Related documents