2010
DOI: 10.1016/j.ast.2010.02.004
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On-ground aircraft control design using a parameter-varying anti-windup approach

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Cited by 38 publications
(23 citation statements)
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“…However, only a few articles address the problem in case of LPV systems [27], [28], [29]. Using the general framework introduced in [30], an AW compensation scheme is proposed to fit the system definition given in the previous subsection.…”
Section: B Anti-windup Compensationmentioning
confidence: 99%
“…However, only a few articles address the problem in case of LPV systems [27], [28], [29]. Using the general framework introduced in [30], an AW compensation scheme is proposed to fit the system definition given in the previous subsection.…”
Section: B Anti-windup Compensationmentioning
confidence: 99%
“…State feedback synthesis is performed, which remains tractable even for eight polytopic scheduling parameters. In [138], approximations based on physical insight are used to reduce the LFT scheduling block's size from 201 × 201 to 7 × 7.…”
Section: B Design Challengesmentioning
confidence: 99%
“…Several methods have been developed to cope with this saturation problem using LMI approaches as given by Tarbouriech and Turner, Do et al, and Roos et al in [14], [15], [16]. Anti-windup used for PID controllers have been investigated by Hippe, Bohn and Atherton, Glattfelder and Schaufelberger in [17], [18], [19].…”
Section: Introductionmentioning
confidence: 99%