Stable inversion and parameter variation
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L.R. Hunt; Viswanath Ramakrishna; George Meyer
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Article
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1998
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Elsevier Science
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English
β 79 KB
As part of the process of automatically guiding an aircraft, we have been successful in using stable inversion to compute a desired bounded state trajectory and corresponding bounded control. In addition to this feedforward control, we must also construct a regulator to address modeling errors and d