Two-Aircraft optimal control problem. The in-flight noise reduction
| dc.creator | Nahayo, Fulgence | |
| dc.creator | Khardi, Salah | |
| dc.creator | Haddou,Mounir | |
| dc.creator | Et al. | |
| dc.date | 2025-01-09T08:57:14Z | |
| dc.date | 2025-01-09T08:57:14Z | |
| dc.date | 2012 | |
| dc.date.accessioned | 2025-06-24T03:53:04Z | |
| dc.description | Article | |
| dc.description | The aim of this paper is to present and solve a mathematical model of a two-aircraft optimal control problem reducing the noise on the ground during the approach. The mathematical modelization of this problem is a non-convex optimal control governed by ordinary non-linear differential equations. To solve this problem, A direct method and a Runge-Kutta RK4 discretization schema are used. This discretization schema is chosed because it is a sufficiently high order and it does-not require computation of the partial derivatives of the aircraft dynamic. The Nonlinear Interior point Trust Region Optimization solver KNITRO is applied. A large set of numerical experiments is presented. The obtained results give feasible trajectories with a significant noise reduction. | |
| dc.format | application/pdf | |
| dc.identifier | https://repository.ub.edu.bi/handle/123456789/1302 | |
| dc.identifier.uri | https://repository.bernet.edu.bi/handle/123456789/842 | |
| dc.publisher | ResearchGate | |
| dc.title | Two-Aircraft optimal control problem. The in-flight noise reduction |