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A comparison of two multi-variable integrator windup protection schemesTwo methods are examined for limit and integrator wind-up protection for multi-input, multi-output linear controllers subject to actuator constraints. The methods begin with an existing linear controller that satisfies the specifications for the nominal, small perturbation, linear model of the plant. The controllers are formulated to include an additional contribution to the state derivative calculations. The first method to be examined is the multi-variable version of the single-input, single-output, high gain, Conventional Anti-Windup (CAW) scheme. Except for the actuator limits, the CAW scheme is linear. The second scheme to be examined, denoted the Modified Anti-Windup (MAW) scheme, uses a scalar to modify the magnitude of the controller output vector while maintaining the vector direction. The calculation of the scalar modifier is a nonlinear function of the controller outputs and the actuator limits. In both cases the constrained actuator is tracked. These two integrator windup protection methods are demonstrated on a turbofan engine control system with five measurements, four control variables, and four actuators. The closed-loop responses of the two schemes are compared and contrasted during limit operation. The issue of maintaining the direction of the controller output vector using the Modified Anti-Windup scheme is discussed and the advantages and disadvantages of both of the IWP methods are presented.
Document ID
19940019117
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mattern, Duane
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1993
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:194436
NASA-CR-194436
AIAA PAPER 93-3812
E-8283
Report Number: NAS 1.26:194436
Report Number: NASA-CR-194436
Report Number: AIAA PAPER 93-3812
Report Number: E-8283
Meeting Information
Meeting: 1993 AIAA Guidance, Navigation, and Control Conference
Location: Monterey, CA
Country: United States
Start Date: August 9, 1993
End Date: August 11, 1993
Sponsors: AIAA
Accession Number
94N23590
Funding Number(s)
PROJECT: RTOP 505-62-50
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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