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The Continuous State Control of Flight Environment Testbed Based on State Feedback and LPV

  • Yuebin Lun
  • , Honglun Wang*
  • , Song Zhang
  • , Zhihong Dan
  • , Qiumeng Qian
  • , Xitong Pei
  • , Zhiyuan Yang
  • *Corresponding author for this work
  • Beihang University
  • Aero Engine Corporation of China

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

Abstract

Flight environment testbed (FET) of Altitude Ground Test Facilities (AGTF) is gradually become the main method of engine testing and simulation. FET is a two-input two-output nonlinear system, and there is a large coupling between the two input and output channels. At present, there are few researches on decoupling of the FET system, so we propose to use the classical state feedback method to achieve it. Considering that the simulation of FET is often a continuous task profile, the linear parameter varying (LPV) is combined with state feedback control in this study to realize continuous state control. The linearization of the system and the LPV will generate certain errors, we propose to add the extended state observer (ESO) to estimate and compensate the errors. Finally, the effectiveness of the proposed method is proved by comparing with the traditional PID method.

Original languageEnglish
Title of host publicationProceedings of 2021 International Conference on Autonomous Unmanned Systems, ICAUS 2021
EditorsMeiping Wu, Yifeng Niu, Mancang Gu, Jin Cheng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages1055-1063
Number of pages9
ISBN (Print)9789811694912
DOIs
StatePublished - 2022
EventInternational Conference on Autonomous Unmanned Systems, ICAUS 2021 - Changsha, China
Duration: 24 Sep 202126 Sep 2021

Publication series

NameLecture Notes in Electrical Engineering
Volume861 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Autonomous Unmanned Systems, ICAUS 2021
Country/TerritoryChina
CityChangsha
Period24/09/2126/09/21

Keywords

  • Decoupling control
  • Extended state observer (ESO)
  • Flight environment testbed (FET)
  • Linear parameter varying (LPV)
  • State feedback

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