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dc.contributor.authorYen, S.D.en_US
dc.date.accessioned2007-05-23T10:03:01Z
dc.date.available2007-05-23T10:03:01Z
dc.date.issued1996en_US
dc.identifier.urihttp://hdl.handle.net/1903/5818
dc.description.abstractThe mixed H2 /H∞ problem arises as one means to achieve robust good performance for a controlled linear time-invariant system. The idea is to achieve H2 optimal performance subject to an H∞ bound as robustness. It has been difficult to find good algorithms for solving this problem. In this study the problem was transformed into a bilinear matrix inequality problem (BMI). Solving the BMI by the method of centers was shown to be complicated by discontinuities resulting from the unobservability of the closed-loop system. Transforming the BMI problem into a lattice of BMI subproblems makes it possible to avoid the discontinuity and solve the original problem. A robust flight control system for the F-14 is included as an example of the algorithm.en_US
dc.format.extent5152972 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; PhD 1996-14en_US
dc.subjectaircraften_US
dc.subjectcomputer aided designen_US
dc.subjectlinear systemsen_US
dc.subjectoptimal controlen_US
dc.subjectoptimizationen_US
dc.subjectsystem theoryen_US
dc.subjectIntelligent Control Systemsen_US
dc.titleMixed H2 /H∞ Optimization: A BMI Solutionen_US
dc.typeDissertationen_US
dc.contributor.departmentISRen_US


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