Please use this identifier to cite or link to this item: https://scholarbank.nus.edu.sg/handle/10635/111606
Title: Mixed H2/H∞ sub-optimization approach for integrated aircraft/controller design
Authors: Liao, F. 
Lum, K.Y. 
Wang, J.L.
Keywords: Integrated aircraft/controller design
Linear matrix inequalities(LMIS)
Mixed H 2/H∞ control
Optimization
Parameter-dependent
Polytopic uncertainty
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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