A comparative study on optimal transient control of aircraft engines

Date

2016

Author

Gao, Yang
Wang, Jiqiang
Wu, Xin
Ye, Zhifeng
Hu, Zhongzhi
Dimirovski, Georgi M.

Metadata

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Citation

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

Abstract

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.

Source

Chinese Intelligent Systems Conference

Volume

1

URI

https://doi.org/10.1007/978-3-662-48386-2_22
http://hdl.handle.net/11376/3167

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