2022
DOI: 10.1007/s42401-022-00143-z
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Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft

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“…The integral term must be forced to zero every time the control error crosses or is equal to zero. This eliminates the need for the regulator to drive the system to have the same error integral in the opposite direction as the disturbance 40 .…”
Section: Introductionmentioning
confidence: 99%
“…The integral term must be forced to zero every time the control error crosses or is equal to zero. This eliminates the need for the regulator to drive the system to have the same error integral in the opposite direction as the disturbance 40 .…”
Section: Introductionmentioning
confidence: 99%