NASA NTRS · 19750050828
Design implementation and control of MRAS error dynamics
Abstract
Use is made of linearized error characteristic equation for model-reference adaptive systems to determine a parameter adjustment rule for obtaining time-invariant error dynamics. Theoretical justification of error stability is given and an illustrative example included to demonstrate the utility of the proposed technique.
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Colburn, B. K., Boland, J. S., III. 1974-01-01. Design implementation and control of MRAS error dynamics. https://ntrs.nasa.gov/citations/19750050828
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