Design and analysis of robust fault diagnosis schemes for a simulated aircraft model

DOI10.1155/2008/274313zbMath1229.93063OpenAlexW2159037957WikidataQ58645461 ScholiaQ58645461MaRDI QIDQ983345

W. Geri, Silvio Simani, Mario Benini, Paolo Castaldi, Marcello Bonfè

Publication date: 22 July 2010

Published in: Journal of Control Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2008/274313

zbMATH Keywords

robustnessreliabilityMonte Carlo analysissensor fault detection and isolationlinear polynomial method

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Design techniques (robust design, computer-aided design, etc.) (93B51) Linear systems in control theory (93C05)

Related Items (2)

A new aerodynamic decoupled frequential FDIR methodology for satellite actuator faults ⋮ Fault diagnosis in dynamic systems using fuzzy interacting observers

Cites Work

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• Observer-based approach to fault detection and isolation for nonlinear systems
• A geometric approach to nonlinear fault detection and isolation
• A direct/functional redundancy scheme for fault detection and isolation on an aircraft
• Fault detection and isolation for on‐board sensors of a general aviation aircraft

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