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Studies of a proportional-integral implicit modelfollowing control law are presented. The research focuses on the ability of the control law to recover the performance of a failed system to its pre-failure level. Properties of the implicit model-following strategy are examined, and conditions for control reconfiguration are stated. The control law is applied to the lateral-directional model of a fighter aircraft, and control restructuring is shown for changes in control and system matrices. It is concluded that the implicit-model following scheme is a good candidate for control reconfiguration.
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Huang et al. (1990) studied this question.
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