Fuzzy Control for Aircraft Engine: Dynamics Clustering Modeling, Compensation and Hardware-in-Loop Experimental Verification

This paper presents an integrated framework for aircraft engines, which consists of three phases: modeling, control, and experimental testing. The engine is formulated as an uncertain T–S fuzzy model. By a hierarchical dynamical parameter clustering, the number and premise variables of fuzzy rules a...

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Bibliographic Details
Main Authors: Muxuan Pan, Hao Wang, Chenchen Zhang, Yun Xu
Format: Article
Language:English
Published: MDPI AG 2024-07-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/11/8/610