Cascade LADRC for hypersonic vehicle with rigid-aeroservoelasticity-sloshing coupling

Wenhui Ma, Kang Chen, Xiaoxi Du, Wenxing Fu

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

1 Scopus citations

Abstract

In this paper, active disturbance rejection control technique is presented for the rigid-aeroservoelasticity(ASE)-sloshing hypersonic vehicle model subject to uncertainties and external disturbance. The statically unstable hypersonic vehicle model outlined here takes into accounts the interactions between liquid sloshing and flexible structure of aircraft. In order to overcome the high nonlinearity, strong coupling and uncertain factors, cascade linear active disturbance rejection controller(LADRC) is utilized to estimate and eliminate internal uncertainness and exogenous disturbances. Finally, simulation results show that the effectiveness of the proposed controller which is validated by the nonlinear model and the proposed method exhibits promising robustness to mismatched uncertainties.

Original languageEnglish
Title of host publication2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence, ICUSAI 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages216-221
Number of pages6
ISBN (Electronic)9781728158594
DOIs
StatePublished - Nov 2019
Event2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence, ICUSAI 2019 - Xi'an, China
Duration: 22 Nov 201924 Nov 2019

Publication series

Name2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence, ICUSAI 2019

Conference

Conference2019 IEEE International Conference on Unmanned Systems and Artificial Intelligence, ICUSAI 2019
Country/TerritoryChina
CityXi'an
Period22/11/1924/11/19

Keywords

  • Aeroservoelasticity
  • Cascade LADRC
  • Hypersonic vehicle
  • Liquid sloshing

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