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- W1970191471 abstract "This paper presents a new methodology to solve the optimization problem of integrated aircraft/dynamic output-feedback controller design where both polytopic model uncertainties and multi-missions are considered. This design optimization is based on mixed H 2 / H ∞ performance requirement. According to the projection lemma, the integrated design optimization problem is separated into aircraft parameter optimization problem and controller optimization problem. An LMI-based sub-optimization approach is proposed for the aircraft parameter design. Then for the obtained sub-optimal aircraft parameters, an optimization approach is given to solve for the dynamic output-feedback controllers corresponding to different missions." @default.
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- W1970191471 date "2005-01-01" @default.
- W1970191471 modified "2023-09-26" @default.
- W1970191471 title "MIXED H2/H∞ SUB-OPTIMIZATION APPROACH FOR INTEGRATED AIRCRAFT/CONTROLLER DESIGN" @default.
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- W1970191471 doi "https://doi.org/10.3182/20050703-6-cz-1902.01978" @default.
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