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SDRE optimal sliding mode guidance law design with attack angle constraint

  • Yuan Sheng Li
  • , Xin Zhao
  • , Si Hong She
  • , Meng Chen Ma
  • , Shen Min Song
  • System Engineering Research Institute
  • Harbin Institute of Technology

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

Abstract

This paper presents an analysis for two-dimensional terminal guidance problem considering target maneuvering and missile autopilot characteristics. A State Dependent Riccati Equation(SDRE) optimal guidance law with attack angle constraint for target non-meneuvering is designed based on SDRE method. Based on the non singular terminal sliding mode surface, a SDRE optimal adaptive non singular terminal sliding mode guidance law is proposed using SDRE method for target maneuvering. The stability of the closed-loop system with respect to the proposed control scheme is proved via Lyapunov theory, and the results of numerical simulations are presented to demonstrate the effectiveness of the proposed approach.

Original languageEnglish
Title of host publicationProceedings of the 38th Chinese Control Conference, CCC 2019
EditorsMinyue Fu, Jian Sun
PublisherIEEE Computer Society
Pages3815-3820
Number of pages6
ISBN (Electronic)9789881563972
DOIs
StatePublished - Jul 2019
Event38th Chinese Control Conference, CCC 2019 - Guangzhou, China
Duration: 27 Jul 201930 Jul 2019

Publication series

NameChinese Control Conference, CCC
Volume2019-July
ISSN (Print)1934-1768
ISSN (Electronic)2161-2927

Conference

Conference38th Chinese Control Conference, CCC 2019
Country/TerritoryChina
CityGuangzhou
Period27/07/1930/07/19

Keywords

  • Autopilot
  • Guidance law
  • Optimal guidance
  • SDRE
  • Terminal sliding mode

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