An adaptive integral sliding mode FTC scheme for dissimilar redundant actuation system of civil aircraft

DOI10.1080/00207721.2019.1673501zbMath1483.93283OpenAlexW2982275679WikidataQ126977000 ScholiaQ126977000MaRDI QIDQ5025856

Lin Yan, Salman Ijaz, Cun Shi, Fuyang Chen, Mirza Tariq Hamayun

Publication date: 7 February 2022

Published in: International Journal of Systems Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207721.2019.1673501

zbMATH Keywords

control allocationfault tolerant controladaptive integral sliding mode controldissimilar actuation

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Adaptive control/observation systems (93C40) Variable structure systems (93B12)

Related Items (1)

A new actuator fault‐tolerant control for Lipschitz nonlinear system using adaptive sliding mode control strategy

Uses Software

• CVX

Cites Work

• Fault tolerant control schemes using integral sliding modes
• Suboptimal integral sliding mode controller design for a class of affine systems
• Control allocation -- a survey
• Active fault-tolerant control of dissimilar redundant actuation system based on performance degradation reference models
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• Actuator fault robust estimation and fault-tolerant control for a class of nonlinear descriptor systems
• On scaled projections and pseudoinverses
• Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure
• Active fault tolerant control design for reusable launch vehicle using adaptive sliding mode technique
• Sliding mode observers for fault detection and isolation
• Nonlinear robust fault reconstruction and estimation using a sliding mode observer
• Nonlinear Integral-Type Sliding Surface for Both Matched and Unmatched Uncertain Systems
• Analysis and design of integral sliding manifolds for systems with unmatched perturbations
• Design and Analysis of an Integral Sliding Mode Fault-Tolerant Control Scheme
• Extended state observer-based motion synchronisation control for hybrid actuation system of large civil aircraft

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