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Switching Anti-windup Synthesis for Linear Systems Subject to Asymmetric Input Magnitude and Rate Saturation: Application to Aircraft Engines

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Date of Publication:2024-08-28

Journal:IEEE Transactions on Aerospace and Electronic Systems

Volume:60

Issue:2

Page Number:1924-1936

ISSN No.:0018-9251

Key Words:ACTUATOR SATURATION; AMPLITUDE; ATTITUDE-CONTROL; DESIGN METHOD; MODEL-PREDICTIVE CONTROL; SPACECRAFT; STABILITY

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