Skip to Main content Skip to Navigation
Journal articles

Optimal control of two-commercial aircraft dynamic system during approach

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.
Complete list of metadatas

Cited literature [37 references]  Display  Hide  Download
Contributor : Ifsttar Cadic <>
Submitted on : Wednesday, May 28, 2014 - 2:53:13 PM
Last modification on : Wednesday, June 20, 2018 - 3:58:02 PM
Document(s) archivé(s) le : Monday, April 10, 2017 - 7:06:26 PM


Files produced by the author(s)


  • HAL Id : hal-00987121, version 1



Fulgence Nahayo, Salah Khardi, Mounir Haddou. Optimal control of two-commercial aircraft dynamic system during approach. General Mathematics Notes, 2011, 3 (2), pp. 27-49. ⟨hal-00987121⟩



Record views


Files downloads