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Cited article:

A Novel Method on Min–Max Limit Protection for Aircraft Engine Control

Wenjun Shu, Bing Yu, Hongwei Ke

MATEC Web of Conferences, 166 (2018) 04002

Published online: 2018-04-23

DOI: https://doi.org/10.1051/matecconf/201816604002

PDF (678 KB)
References

This article has been cited by the following article(s):

Multi-Model Structured H-Infinity Design of a Robust and Aggressive Turbofan Jet Engine Controller

Patrick Authié
ASME Letters in Dynamic Systems and Control 2 (2) (2022)
https://doi.org/10.1115/1.4052916