A New Method of Missile Agile Turning Using Terminal Sliding Mode Control

Shuai Xie, Yong Yu*, Zheng Li, Jianqiao Yu

*Corresponding author for this work

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

Abstract

This paper addresses the implementation issues of missile agile turning and proposes a novel solution using a flexible parachute/rudder scheme. It is compared and validated through simulation with pure rudder scheme and reaction-jet/rudder scheme. To address the highly nonlinear, uncertain, and rapidly time-varying dynamics of agile turning, a non-singular terminal sliding mode method is employed to ensure that the control system tracks the pitch angle command within a finite time. By establishing a longitudinal plane dynamics model and designing the controller, the agile turning is simulated and verified. The simulation results demonstrate that the flexible parachute/rudder scheme effectively achieves turning and the turning performance is comparable to the reaction-jet/rudder scheme.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 2
EditorsLiang Yan, Haibin Duan, Yimin Deng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages468-475
Number of pages8
ISBN (Print)9789819622030
DOIs
Publication statusPublished - 2025
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2024 - Changsha, China
Duration: 9 Aug 202411 Aug 2024

Publication series

NameLecture Notes in Electrical Engineering
Volume1338 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2024
Country/TerritoryChina
CityChangsha
Period9/08/2411/08/24

Keywords

  • Flexible parachute-rudder control
  • Missile agile turning
  • Terminal sliding mode

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