Fault detection using differential flatness in flight guidance systems - Archive ouverte HAL Accéder directement au contenu
Communication Dans Un Congrès Année : 2007

Fault detection using differential flatness in flight guidance systems

(1) , (2) , (1) , (1, 3) , (2) , (2)
1
2
3

Résumé

In this paper, flight guidance dynamics are shown to be implicit differentially flat with respect to the inertial position of an aircraft. This proves the existence of a set of relations between these flat outputs and the state variables representative of flight guidance dynamics and between these flat outputs and the basic inputs to flight guidance dynamics. A neural network is introduced to obtain, from the actual trajectory, nominal flight parameters which can be compared with actual values to detect abnormal behaviour.
Fichier principal
Vignette du fichier
363.pdf (331.94 Ko) Télécharger le fichier
Origine : Fichiers éditeurs autorisés sur une archive ouverte
Loading...

Dates et versions

hal-00938151 , version 1 (23-06-2014)

Identifiants

Citer

Wen Chi Lu, Rabah Fellouah, Geanina Andrei, Nan Zhang, Felix Mora-Camino, et al.. Fault detection using differential flatness in flight guidance systems. CISIS 2007, 1st International Conference on Complex, Intelligent and Software Intensive Systems, Apr 2007, Vienna, Austria. pp 155-159, ⟨10.1109/CISIS.2007.24⟩. ⟨hal-00938151⟩
151 Consultations
172 Téléchargements

Altmetric

Partager

Gmail Facebook Twitter LinkedIn More