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Data-Based Spacecraft Rendezvous Control by SINDy

  • Jin Tan
  • , Guang Ren Duan
  • , Mingming Shi*
  • , Bin Li
  • *Corresponding author for this work
  • Sichuan University

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

Abstract

In this paper, we demonstrate a new model identification method for spacecraft rendezvous with few amounts of data and low computational burdens by utilizing sparse identification for nonlinear dynamical (SINDy). Besides, a control scheme composed of SINDy and Linear Quadratic Regulator (LQR) is demonstrated, which aims to enhance the robustness and optimality simultaneously. The numerical results show the effectiveness of the proposed control scheme for spacecraft rendezvous mission.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 5
EditorsLiang Yan, Haibin Duan, Yimin Deng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages412-421
Number of pages10
ISBN (Print)9789819622153
DOIs
StatePublished - 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
Volume1341 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

  • linear quadratic regulator
  • spacecraft rendezvous
  • sparse identification for nonlinear dynamical

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