Intelligent robust control for aviation electric fuel pump based on second order integral sliding mode with UDE-Reference-Cited by-同舟云学术

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Intelligent robust control for aviation electric fuel pump based on second order integral sliding mode with UDE

Published:2024-05 Issue:8 Volume:361 Page:106811
ISSN:0016-0032
Container-title:Journal of the Franklin Institute
language:en
Short-container-title:Journal of the Franklin Institute

Author:

Xiao Lingfei^ORCID,Han Zirui^ORCID,Ma Leiming^ORCID,Jiang Bin^ORCID

Funder

Nanjing University of Aeronautics and Astronautics

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference43 articles.

1. The more electric aero-engine: A general overview from an engine manufacturer;Provost,2002

2. A scientometric analysis and critical review of gas turbine aero-engines control: From whittle engine to more-electric propulsion;Mohammadi;Meas. Control.,2021

3. Research on Structure Design and Control System Development of Electric Fuel Pump;Liu,2017

4. Robust control for electric fuel pump with variant nonlinear loads based on a new combined sliding mode surface;Ding;Int. J. Control Autom. Syst.,2019

5. Research on System Modeling and Control of Aviation Electric Fuel Pump;Li,2018

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