Optimal control of two-commercial aircraft dynamic system during approach

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.

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Additional Info

Field Value
Source General Mathematics Notes
Author Nahayo, Fulgence, Khardi, Salah, Haddou, Mounir
Maintainer CCSD
Last Updated May 5, 2026, 12:10 (UTC)
Created May 5, 2026, 12:10 (UTC)
Identifier hal-00987121
Language en
Rights https://about.hal.science/hal-authorisation-v1/
contributor Université du Burundi = University of Burundi [Bujumbura]
creator Nahayo, Fulgence
date 2011-01-01T00:00:00
harvest_object_id 45a22381-2881-4e8c-a748-3653b1f9571e
harvest_source_id 3374d638-d20b-4672-ba96-a23232d55657
harvest_source_title test moissonnage SELUNE
metadata_modified 2026-04-04T00:00:00
set_spec type:ART