Direct Performance Control Method for Turbofan Afterburning Control with a Nonlinear Fuel Supply System-Reference-Cited by-同舟云学术

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Direct Performance Control Method for Turbofan Afterburning Control with a Nonlinear Fuel Supply System

Published:2023-06-23 Issue:1 Volume:25 Page:293-307
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Xi Zhihua^ORCID,Chen Ming,Zhang Haibo,Wang Yong

Funder

National Science and Technology Major Project

Basic Problem of Intelligent Aero-engine

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-023-00634-z.pdf

Reference19 articles.

1. Mattingly JD, Mattingly JD, Mattingly JD (2015) Aircraft engine design, 2nd edn. AIAA

2. Jaw LC, Mattingly JD (2009) Aircraft engine controls. American Institute of Aeronautics and Astronautics, New York

3. Lin Z, Ding F (2010) Afterburning fuel flow optimal control. Propulsion technology 31(005):572–575

4. Tudosie AN. Afterburning Control System Based on Fuel Injection Dosage System with Respect to the Turbine's Pressure Ratio

5. Knoll Z, Gang T (2015) Multivariable adaptive LQ control of jet engines. Proceedings of the American Control Conference 2015:1193–1198

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Model-based deduction learning control: A novel method for optimizing gas turbine engine afterburner transient;Energy;2024-04

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