DocumentCode :
133131
Title :
Reduced order flutter modeling based on the Hammerstein model with μ-Markov structure and correlation identification method
Author :
Kai-Yew Lum ; Kwok-Leung Lai
Author_Institution :
Dept. of Electr. Eng., Nat. Chi Nan Univ., Puli, Taiwan
fYear :
2014
fDate :
9-12 Sept. 2014
Firstpage :
1691
Lastpage :
1697
Abstract :
This paper presents an approach for reduced order flutter modeling based on the Hammerstein model and system identification. The Hammerstein model considered is prescribed a μ-Markov structure in the linear block, and its identification employs a correlation-based method for separable input processes. This combination of model and identification method has been shown in a previous work to accurately identify the linear block, which is vital to bifurcation analysis. Using computational fluid dynamics data and an experimental benchmark, it is shown that the proposed approach yields better accuracy relative to the benchmark as well as by model validation.
Keywords :
Markov processes; aerodynamics; aerospace components; computational fluid dynamics; reduced order systems; Hammerstein model; Markov structure; computational fluid dynamics; correlation identification method; reduced order flutter modeling; wing aerodynamic response; Aerodynamics; Atmospheric modeling; Benchmark testing; Computational modeling; Correlation; Mathematical model; Read only memory; Hammerstein model; System identification; aerodynamics; reduced-order modeling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
SICE Annual Conference (SICE), 2014 Proceedings of the
Conference_Location :
Sapporo
Type :
conf
DOI :
10.1109/SICE.2014.6935293
Filename :
6935293
Link To Document :
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