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A passive fault tolerant flight control for maximum allowable vertical tail damaged aircraft / Xiaobo Li in Transactions of the ASME . Journal of dynamic systems, measurement, and control, Vol. 134 N° 3 (Mai 2012) 

Public ISBD [article]  in Transactions of the ASME . Journal of dynamic systems, measurement, and control > Vol. 134 N° 3 (Mai 2012) . - 15 p. Titre : A passive fault tolerant flight control for maximum allowable vertical tail damaged aircraft Type de document : texte imprimé Auteurs : Xiaobo Li, Auteur ; Hugh H. T. Liu, Auteur Année de publication : 2012 Article en page(s) : 15 p. Note générale : Dynamic systems Langues : Anglais (eng) Mots-clés : Passive  fault  tolerant  control  Aircraft  Vertical  tail  damage Index. décimale : 629.8 Résumé : This paper investigates a passive fault tolerant control to aircraft that suffers from vertical tail damage. A novel notion of damage degree is introduced to parameterize the damaged flight dynamics model. It is applied to seek the maximum allowable damage degree (tolerance capacity) stabilizable by the proposed passive fault tolerant and backup control under a linearized model. The design algorithms are presented and illustrated through numerical simulations on a Boeing-747 100/200 model. Furthermore, the impact of potential control saturation is taken into account in the proposed design and a set of design parameters are tuned such that the maximum allowable damage degree is bounded, represented as the so-called critical damage degree. DEWEY : 629.8 ISSN : 0022-0434 En ligne : http://asmedl.org/getabs/servlet/GetabsServlet?prog=normal&id=JDSMAA000134000003 [...] [article] A passive fault tolerant flight control for maximum allowable vertical tail damaged aircraft [texte imprimé] / Xiaobo Li, Auteur ; Hugh H. T. Liu, Auteur . - 2012 . - 15 p. Dynamic systems Langues : Anglais (eng) in Transactions of the ASME . Journal of dynamic systems, measurement, and control > Vol. 134 N° 3 (Mai 2012) . - 15 p. Mots-clés : Passive  fault  tolerant  control  Aircraft  Vertical  tail  damage Index. décimale : 629.8 Résumé : This paper investigates a passive fault tolerant control to aircraft that suffers from vertical tail damage. A novel notion of damage degree is introduced to parameterize the damaged flight dynamics model. It is applied to seek the maximum allowable damage degree (tolerance capacity) stabilizable by the proposed passive fault tolerant and backup control under a linearized model. The design algorithms are presented and illustrated through numerical simulations on a Boeing-747 100/200 model. Furthermore, the impact of potential control saturation is taken into account in the proposed design and a set of design parameters are tuned such that the maximum allowable damage degree is bounded, represented as the so-called critical damage degree. DEWEY : 629.8 ISSN : 0022-0434 En ligne : http://asmedl.org/getabs/servlet/GetabsServlet?prog=normal&id=JDSMAA000134000003 [...]