Abstract:Indirect adaptive control for reconfigurable flight control is advocated. Specifically, on-line static system identification using a moving window/batch estimation, is used. The ensuing linear regression is augmented with an intercept to address the effects of trim change associated with the occurrence of a control surface failure. Parameter estimate information is used to adjust the inner loop's control gains and a command derived from the intercept estimate is fed forward to retrim the aircraft automatically… Show more
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