Linear optimal control is applied to a model-following problem where a plant, subject to parameter variations, is required to follow the response of a given model to an arbitrary input. A fixed-gain control configuration is obtained for any model input that provides model for a given set of plant parameters. The sensitivity of the system to plant parameter variations is reduced by formulating a type-one perfect model-folio wing system. The existence of feedforward gains for perfect model following is discussed and the results are applied to an aircraft control problem.
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Sabi J. Asseo (1970) studied this question.
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