Decoupling Controller Design for BTT Missile With Coupled Channels Based on Sliding Mode and Neural Network

Bin Huang, Yongshan Liu*, Siqi Li

*Corresponding author for this work

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

Abstract

Aiming at the serious coupled channels control problem in BTT missile, this paper adopts theories of sliding mode and neural network to design missile controller. Firstly, sliding mode control and neural network are introduced, and the joint equation of states for pitch and yaw channels of BTT missile is established. Secondly, the coupling factors are estimated by the linear extended states observer for decoupling and the control laws of coupled channels are designed. Thirdly, in order to decrease the chattering of sliding mode control, the gain term of sliding mode would be adjusted by RBF neural network online. Finally, the performance and robustness of the designed controller are verified by simulation.

Original languageEnglish
Title of host publicationProceeding - 2021 China Automation Congress, CAC 2021
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages1151-1156
Number of pages6
ISBN (Electronic)9781665426473
DOIs
Publication statusPublished - 2021
Event2021 China Automation Congress, CAC 2021 - Beijing, China
Duration: 22 Oct 202124 Oct 2021

Publication series

NameProceeding - 2021 China Automation Congress, CAC 2021

Conference

Conference2021 China Automation Congress, CAC 2021
Country/TerritoryChina
CityBeijing
Period22/10/2124/10/21

Keywords

  • BTT missile
  • Gain term adjusting
  • Linear extended states observer
  • RBF neural network
  • Sliding mode control

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