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Design of Preview Controller for Aviation Electric Fuel Pump Based on Adaptive Sliding Mode Feedback Linearization.

Authors :
MENG Xiangshuo
XIAO Lingfei
MA Leiming
Source :
Transactions of Nanjing University of Aeronautics & Astronautics; Feb2023, Vol. 40 Issue 1, p47-59, 13p
Publication Year :
2023

Abstract

<i>Copyright of Transactions of Nanjing University of Aeronautics & Astronautics is the property of Editorial Department of Journal of Nanjing University of Aeronautics & Astronautics and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.)

Details

Language :
English
ISSN :
10051120
Volume :
40
Issue :
1
Database :
Complementary Index
Journal :
Transactions of Nanjing University of Aeronautics & Astronautics
Publication Type :
Academic Journal
Accession number :
162298926
Full Text :
https://doi.org/10.16356/j.1005‑1120.2023.01.005