Analysis of the influence of partial fuel transfer line leak on active center of gravity control

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Active center of gravity control can transfer fuel among many fuselage fuel tanks to effectively optimize aircraft center of gravity and gain the potential economic performance benefits. In-flight possible failures in the fuel system may generate direct influences on aircraft center of gravity control. The aim of this article is to investigate the influence of partial fuel transfer line leak on the active center of gravity control system. First, modeling of center of gravity variation due to fuel transfer is presented and then aircraft center of gravity control law based on sliding mode is put forward. Then, detailed simulation analyses of the influence of possible fuel transfer line leak on center of gravity tracking performance are carried out, including different one or two fuel lines leak conditions. Finally, the emergency strategies for the aircraft center of gravity control system to cope with possible failures are concluded and proposed.

Original languageEnglish
Title of host publicationAUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages151-155
Number of pages5
ISBN (Electronic)9781509010875
DOIs
StatePublished - 17 Nov 2016
Event2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China
Duration: 10 Oct 201612 Oct 2016

Publication series

NameAUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

Conference

Conference2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Country/TerritoryChina
CityBeijing
Period10/10/1612/10/16

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