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Koopman Operator-Based Model Predictive Control for Impact Angle Guidance

  • Harbin Institute of Technology
  • Aerospace System Engineering Shanghai

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

Abstract

This paper presents a Koopman operator-based model predictive control (MPC) strategy for impact angle control guidance (IACG) of homing missiles. First, a data-driven Koopman operator is introduced to obtain the globally linearized guidance model of lifted states in the reference coordinate. Then, a Koopman linear model based MPC is designed to solve the IACG problem. Compared with conventional local linearization relying on the small-angle assumption, the proposed Koopman operator-MPC based IACG (KMPC-IACG) law can capture the full nonlinear dynamics more precisely, thus more applicable to the IACG problem involving large maneuvers or under conditions of large terminal constraint angles. Simulation results exhibit excellent performance comparable to the IACG open-loop optimal solution and verify the effectiveness of our method.

Original languageEnglish
Title of host publicationProceedings of the 44th Chinese Control Conference, CCC 2025
EditorsJian Sun, Hongpeng Yin
PublisherIEEE Computer Society
Pages4329-4334
Number of pages6
ISBN (Electronic)9789887581611
DOIs
StatePublished - 2025
Event44th Chinese Control Conference, CCC 2025 - Chongqing, China
Duration: 28 Jul 202530 Jul 2025

Publication series

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

Conference

Conference44th Chinese Control Conference, CCC 2025
Country/TerritoryChina
CityChongqing
Period28/07/2530/07/25

Keywords

  • Data-driven control
  • Homing guidance
  • Impact angle control
  • Koopman operator
  • Model predictive control

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