Mathematical model for advanced CDA and takeoff procedures minimizing aircraft environmental impact
type: Dataset
description: The objective of this paper is to develop a mathematical optimal control model to find and evaluate optimized flight paths in order to minimize aircraft noise levels and fuel consumption during approaches and departures. The developed optimization method and numerical algorithms are given and analyzed. Aircraft flight dynamics and trajectories have been considered. The advanced continuous descent approach CDA has been found to be the optimal approach procedure. Its performance has been presented and discussed in comparison with standard procedures. The merits of optimal take-of flight paths have been also performed and analyzed. Keywords: aircraft noise abatement, fuel consumption, flight path, optimal control.
landing page: International Mathematical Forum
keyword: analyse-mathematique
keyword: avion
keyword: carburant
keyword: infoeu-reposemanticsarticle
keyword: infoinfo-itcomputer-science-csinformation-theory-csit
keyword: journal-articles
keyword: mathematiques
keyword: mathmath-gmmathematics-mathgeneral-mathematics-mathgm
keyword: mathmath-itmathematics-mathinformation-theory-mathit
keyword: sdeesenvironmental-sciencesenvironment-and-society
keyword: voie-de-circulation
issued: 2026-05-05T09:49:51.924118
modified: 2026-05-05T09:49:51.924123
language: en
contact point: Organization
  fn: CCSD

test_moissonnage_selune
type: Agent

Mathematical model for advanced CDA and takeoff procedures minimizing aircraft environmental impact
type: Distribution
format: HTML
access URL: https://hal.science/hal-00999273
issued: 2026-05-05T09:49:51.933566
modified: 2026-05-05T09:49:51.909625