Improvement of Min–Max limit protection in aircraft engine control: An LMI approach-Reference-Cited by-同舟云学术

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Improvement of Min–Max limit protection in aircraft engine control: An LMI approach

Published:2017-09 Issue: Volume:68 Page:214-222
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Imani Amin^ORCID,Montazeri-Gh Morteza

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference18 articles.

1. Control Design for a Generic Commercial Aircraft Engine;Csang,2010

2. Reducing Conservatism in Aircraft Engine Response Using Conditionally Active Min–Max Limit Regulators;May,2012

3. Control of jet engines;Spang;J. Control Eng. Pract.,1999

4. A Modular Aero-Propulsion System Simulation of a Large Commercial Aircraft Engine;DeCastro,2008

5. Aircraft Engine Controls-Design, System Analysis and Health Monitoring;Jaw,2009

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