Abstract
Complex and strong nonlinearity are important characteristics of aero-engines, and they often work in harsh environments. How to design a simple, stable, and small-calculation nonlinear controller applying appropriate nonlinear theory is a great challenge. Aiming at this challenge, a controller design method based on Nonlinear Generalized Minimum Variance (NGMV) be proposed by this paper. The NGMV controller of an aero-engine is designed and implemented, and its excellent control performance is proved by comparison with the traditional PI controller.
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Du, X., Wang, X., Wang, J. (2022). Nonlinear Control Design of Aero-Engine Based on NGMV. In: Jia, Y., Zhang, W., Fu, Y., Yu, Z., Zheng, S. (eds) Proceedings of 2021 Chinese Intelligent Systems Conference. Lecture Notes in Electrical Engineering, vol 803. Springer, Singapore. https://doi.org/10.1007/978-981-16-6328-4_20
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DOI: https://doi.org/10.1007/978-981-16-6328-4_20
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