The Trust Region Sequential Quadratic Programming method applied to two-aircraft acoustic optimal control problem
| dc.contributor.author | Khardi, S. | |
| dc.contributor.author | F. Nahayo | |
| dc.contributor.author | M. Haddou | |
| dc.date.accessioned | 2025-04-22T12:42:16Z | |
| dc.date.available | 2025-04-22T12:42:16Z | |
| dc.date.issued | 2011 | |
| dc.description | Article de recherche scientifique | |
| dc.description.abstract | This paper aims to reduce noise levels of two-aircraft landing simultaneously on approach. Constraints related to stability, performance and ight 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. | |
| dc.identifier.uri | https://repository.ub.edu.bi/handle/123456789/1920 | |
| dc.publisher | Research Gate | |
| dc.title | The Trust Region Sequential Quadratic Programming method applied to two-aircraft acoustic optimal control problem |