A comparative study on optimal transient control of aircraft engines
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Springer
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
Sequential quadratic programming has been widely used in the optimization of transient control of aircraft engine. On the other hand, the study of nonlinear optimization theory and method has been made great advance in recent years, of which active set method is one of the effective measures. In this article, the two algorithms are used to optimize the inputs based on one turbofan engine model. Results from the simulation comparisons of the two algorithms, advantages and disadvantages are given.
Açıklama
Dimiorvski, Georgi M. -- Conference full title: 2015 Chinese Intelligent Systems Conference, IFAC; Seoul; South Korea; 6 July 2008 through 11 July 2008. CISC; Yangzhou; China
Anahtar Kelimeler
Optimization Algorithm, SQP, ASM, Turbofan Engine Model
Kaynak
Chinese Intelligent Systems Conference
WoS Q Değeri
Scopus Q Değeri
Cilt
1
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Künye
Gao, Y., Wang, J. Q., Wu, X., Ye, Z., Hu, Z., Dimirovski, G. M. (2016). A comparative study on optimal transient control of aircraft engines. In Jia Y., Du J., Li H., Zhang W. (Eds.) Proceedings of the 2015 Chinese Intelligent Systems Conference (pp. 205-212). https://doi.org/10.1007/978-3-662-48386-2_22












