Optimal control of two-commercial aircraft dynamic system during approach
NAHAYO ; KHARDI ; HADDOU
Type de document
ARTICLE A COMITE DE LECTURE NON REPERTORIE DANS BDI (ACLN)
Langue
anglais
Auteur
NAHAYO ; KHARDI ; HADDOU
Résumé / 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.
Source
General Mathematics Notes, num. 2, pp. 27-49 p.
Editeur
ICSRS Publication
