Accéder directement au contenu Accéder directement à la navigation
Communication dans un congrès

On-Line Optimization for Fault Tolerant Flight Control

Abstract : In this communication the case in which an aerodynamic actuator failure occurs to an aircraft while it has to perform some guidance maneuver is considered. This problem is dealt with the reassignment of remaining operational actuators in order to perform the required maneuver while maintaining the structural integrity of the aircraft. Nonlinear Inverse Control technique is used to generate online nominal moments along the three axes of the aircraft. Taking into account all material and structural constraints as well as the redundant effects from other actuators, a mathematical programming problem to be solved on-line which related to control reallocation can be formulated. Solution techniques, based on dynamic neural networks, active set methods and interior point methods are discussed and the respective performances are compared.
Type de document :
Communication dans un congrès
Liste complète des métadonnées

Littérature citée [18 références]  Voir  Masquer  Télécharger

https://hal-enac.archives-ouvertes.fr/hal-00930266
Contributeur : Céline Smith Connectez-vous pour contacter le contributeur
Soumis le : mardi 14 janvier 2014 - 15:30:33
Dernière modification le : lundi 4 juillet 2022 - 08:45:49
Archivage à long terme le : : mardi 15 avril 2014 - 16:25:46

Fichier

Zhong_ISAA2013.pdf
Fichiers produits par l'(les) auteur(s)

Identifiants

  • HAL Id : hal-00930266, version 1

Citation

Lunlong Zhong, Felix Mora-Camino. On-Line Optimization for Fault Tolerant Flight Control. ISAA 2013, 3rd International Symposium on Aircraft Airworthiness, Nov 2013, Toulouse, France. ⟨hal-00930266⟩

Partager

Métriques

Consultations de la notice

131

Téléchargements de fichiers

168