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Formation Reconfiguration in Elliptic Orbit for Spacecraft Without the Radial Thrust

  • Jiang Shao
  • , Qingrui Zhou
  • , Nan Xiao
  • , Dong Ye*
  • , Zhaowei Sun
  • *Corresponding author for this work
  • Harbin Institute of Technology
  • China Aerospace Science and Technology Corporation

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

Abstract

The feasibility of formation reconfiguration for underactuated spacecraft in elliptic orbits is investigated in this paper. Based on the coupling relationship of the relative orbital states, the linear transformations are performed on the original state vectors to generate two second-order state vectors. We construct an underactuated auxiliary system to compensate for the input saturation for the Tschauner-Hempel equation and thus design an underactuated saturated controller. The stable reconfiguration accuracies of the state variables of the underactuated system are derived based on the Lyapunov method.

Original languageEnglish
Title of host publicationAdvances in Guidance, Navigation and Control - Proceedings of 2022 International Conference on Guidance, Navigation and Control
EditorsLiang Yan, Haibin Duan, Yimin Deng, Liang Yan
PublisherSpringer Science and Business Media Deutschland GmbH
Pages5103-5112
Number of pages10
ISBN (Print)9789811966125
DOIs
StatePublished - 2023
EventInternational Conference on Guidance, Navigation and Control, ICGNC 2022 - Harbin, China
Duration: 5 Aug 20227 Aug 2022

Publication series

NameLecture Notes in Electrical Engineering
Volume845 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Guidance, Navigation and Control, ICGNC 2022
Country/TerritoryChina
CityHarbin
Period5/08/227/08/22

Keywords

  • Elliptic orbit
  • Formation reconfiguration
  • Saturated controller
  • Stable reconfiguration accuracy
  • Underactuated spacecraft

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