Study on Identification Method for Parameter Uncertainty Model of Aero Engine
The linear model of an aero engine is effective in a small range of the neighborhood of equilibrium points. According to this problem, the identification method for the parameter uncertain linear model of the aero engine was proposed. The identification problem is solved by calculating nonlinear pro...
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Main Authors: | Jie Bai, Shuai Liu, Wei Wang |
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Format: | Article |
Language: | English |
Published: |
Wiley
2019-01-01
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Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2019/6015270 |
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