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|Title:||Mixed H2/H∞ sub-optimization approach for integrated aircraft/controller design||Authors:||Liao, F.
|Keywords:||Integrated aircraft/controller design
Linear matrix inequalities(LMIS)
Mixed H 2/H∞ control
|Issue Date:||2005||Citation:||Liao, F.,Lum, K.Y.,Wang, J.L. (2005). Mixed H2/H∞ sub-optimization approach for integrated aircraft/controller design. IFAC Proceedings Volumes (IFAC-PapersOnline) 16 : 103-108. ScholarBank@NUS Repository.||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 H2/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. Copyright © 2005 IFAC.||Source Title:||IFAC Proceedings Volumes (IFAC-PapersOnline)||URI:||http://scholarbank.nus.edu.sg/handle/10635/111606||ISBN:||008045108X||ISSN:||14746670|
|Appears in Collections:||Staff Publications|
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