A Simplified Backstepping Design for 3D Time-based Aircraft Relative Guidance

Thierry Miquel 1, 2 Felix Antonio Claudio Mora-Camino 3 Francis Casaux 1 Jean-Marc Loscos 1
1 DGAC - Direction Générale de l'Aviation Civile
2 LAAS - Laboratoire d'analyse et d'architecture des systèmes [Toulouse]
3 LAAS-DISCO - Équipe DIagnostic, Supervision et COnduite
LAAS - Laboratoire d'analyse et d'architecture des systèmes [Toulouse]
Abstract : The delegation to the flight crew of some tasks currently performed by air traffic controllers provides new perspectives to potentially increase air traffic control capacity. The objective of this communication is to provide technical insight into the airborne devices and algorithms which may be used to automatically perform merging and station keeping operations. Indeed, these maneuvers in the field of civil aviation seem difficult to be performed manually and may result in this case in an increase of the flight crew workload. Nevertheless new automated functions onboard aircraft could help to overcome this limitation. This paper investigates the design of a new autopilot mode dedicated to merging and station keeping maneuvers behind a leading aircraft. The proposed relative guidance law considers a 3-D relative motion, including constant wind and lateral, longitudinal and vertical control. It is based on vectorial backstepping and takes advantage of the skewsymmetric matrix which appears in the relative motion equations. An alternative "simplified" design based on a matrix form of the Young's inequality is also presented in order to simplify the computation of the guidance law. Then, an illustrative example is discussed and conclusions are raised.
Type de document :
Communication dans un congrès
AIAA GNC 2004, AIAA Guidance, Navigation and Control Conference and Exhibit, Aug 2004, Providence, United States. pp xxxx, 2004, 〈10.2514/6.2004-4993〉
Liste complète des métadonnées

Littérature citée [8 références]  Voir  Masquer  Télécharger
https://hal-enac.archives-ouvertes.fr/hal-00998749
Contributeur : Céline Smith <>
Soumis le : lundi 2 juin 2014 - 16:15:49
Dernière modification le : mercredi 12 décembre 2018 - 15:25:07
Document(s) archivé(s) le : mardi 2 septembre 2014 - 12:46:33

Fichier

AIAA-2004-4993-104.pdf
Fichiers éditeurs autorisés sur une archive ouverte

Identifiants

Collections

MAIAA | MAIAA-AUTO | ENAC | LAAS | LAAS-DISCO | LAAS-DECISION-ET-OPTIMISATION | UNIV-TLSE3 | TDS-MACS | INSA-TOULOUSE | DGAC

Citation

Thierry Miquel, Felix Antonio Claudio Mora-Camino, Francis Casaux, Jean-Marc Loscos. A Simplified Backstepping Design for 3D Time-based Aircraft Relative Guidance. AIAA GNC 2004, AIAA Guidance, Navigation and Control Conference and Exhibit, Aug 2004, Providence, United States. pp xxxx, 2004, 〈10.2514/6.2004-4993〉. 〈hal-00998749〉

Exporter

BibTeX TEI DC DCterms EndNote

Partager

Métriques

Consultations de la notice

198

Téléchargements de fichiers

90

Picto

Contact  : publications@enac.fr