Nonlinear control study on aircraft engine using a generalized minimum variance approach

With the requirements of the advanced propulsion systems for aircraft control performance increasing, it has attracted the attention to design more efficient controller that is based on the nonlinear model over the flight envelope directly. A nonlinear aircraft engine control method based on general...

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Bibliographic Details
Main Authors: Bing Yu, Yang Gao, Jiqiang Wang
Format: Article
Language:English
Published: SAGE Publishing 2016-09-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814016667383