2013
DOI: 10.1109/tfuzz.2012.2224872
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Fuzzy-Model-Based Fault-Tolerant Design for Nonlinear Stochastic Systems Against Simultaneous Sensor and Actuator Faults

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Cited by 214 publications
(134 citation statements)
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“…Step 4: Compute matrices N and H based on Equation 18. Consequently, observer matrices N, T, H, M, and F are all computed, and the fault reconstruction observer can be constructed as in Equation 5.…”
Section: Corollarymentioning
confidence: 99%
See 1 more Smart Citation
“…Step 4: Compute matrices N and H based on Equation 18. Consequently, observer matrices N, T, H, M, and F are all computed, and the fault reconstruction observer can be constructed as in Equation 5.…”
Section: Corollarymentioning
confidence: 99%
“…Various effective techniques, such as adaptive technique, [6][7][8] sliding-mode observer approach using equivalent output injection signal to explicitly reconstruct fault signals, [9][10][11][12] learning observer method, 13,14 intermediate estimator method, 15,16 the descriptor observer approach, [17][18][19] and so on, have been proposed for fault estimation problem. Recently, the proportional and integral observer (PIO) method has been addressed in the works of Youssef et al 20 and Li and Zhu 21 to simultaneously estimate system states and system faults.…”
Section: Introductionmentioning
confidence: 99%
“…Among this work, T-S fuzzy systems and Markovian jump systems are two representative classes of dynamical systems. Over the past decades, many meaningful results have been published on the sliding mode control of either T-S fuzzy systems [10,11,12,13] or Markovian jump systems [14,15,16,17,18,19,20]. However, relatively little attention has been focused on research into sliding mode control for composite systems comprising the two classes of systems, namely Markovian jump T-S fuzzy systems [21,22], despite their wide application [23,24,25,26].…”
Section: Introductionmentioning
confidence: 99%
“…[17][18][19] To mention a few, a quaternion-based attitude tracking control law is proposed for rigid satellite in the presence of unknown inertia matrix. 20 A robust control strategy is developed for rigid body satellite to achieve high-precision attitude tracking, where time-varying mass and unknown external disturbance are considered together.…”
Section: Introductionmentioning
confidence: 99%