Fault-tolerant control based Super-Twisting algorithm for the diesel engine air path subject to loss-of-effectiveness and additive actuator faults
نویسندگان
چکیده
منابع مشابه
Finite-time fault tolerant attitude control for over-activated spacecraft subject to actuator misalignment and faults
A finite-time attitude compensation control scheme is developed for an over-activated rigid spacecraft subject to actuator faults, misalignment, external disturbances and uncertain inertia parameters. The controller is synthesised based on the sliding mode control theory, and guarantees the finite-time reachability of the system states. A sufficient condition for the controller to accommodate m...
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1Hautes Etudes d’Ingénieur, Centre de Recherche en Informatique, Signal et Automatique de Lille (CRIStAL), 13 rue de Toul, 59046 Lille, France 2Lille 1 University, Centre de Recherche en Informatique, Signal et Automatique de Lille (CRIStAL), rue Paul Langevin, 59655 Villeneuve d’Ascq, France 3Department of Engineering & Design, University of Sussex, Room 2D3, Richmond Building, Brighton BN1 9Q...
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ژورنال
عنوان ژورنال: Applied Mathematical Modelling
سال: 2015
ISSN: 0307-904X
DOI: 10.1016/j.apm.2014.12.047