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A Passive Fault Tolerant Flight Control for Maximum Allowable Vertical Tail Damaged Aircraft

Author
XIAOBO LI1 ; LIU, Hugh H. T1
[1] Flight Systems and Control Group, Institute for Aerospace Studies, University of Toronto, Toronto, ON, M3H 5T6, Canada
Source

Journal of dynamic systems, measurement, and control. 2012, Vol 134, Num 3 ; 031006.1-031006.15 ; ref : 25 ref

CODEN
JDSMAA
ISSN
0022-0434
Scientific domain
Control theory, operational research; Mechanical engineering
Publisher
American Society of Mechanical Engineers, New York, NY
Publication country
United States
Document type
Article
Language
English
Keyword (fr)
Aérodynamique Aéronef Borne supérieure Commande vol Conception ingénierie Endommagement Modèle dynamique Modélisation Saturation Système passif Système tolérant les pannes Tolérance faute
Keyword (en)
Aerodynamics Aircraft Upper bound Flight control Engineering design Damage Dynamic model Modelling Saturation Passive system Fault tolerant system Fault tolerance
Keyword (es)
Cota superior Control vuelo Concepción ingeniería Modelo dinámico Sistema pasivo Sistema tolerando faltas
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40G Fluid dynamics / 001B40G85 Applied fluid mechanics / 001B40G85B Aerodynamics

Discipline
Physics : fluid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
25857030

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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