Characteristic Model-Based Adaptive Control for Spacecraft Rendezvous and Proximity Operations

  • Yao Lu
  • , Yingmin Jia*
  • *Corresponding author for this work

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

Abstract

In this paper, the spacecraft relative motion control problem with actuator saturation is studied for rendezvous and proximity missions. The decoupled characteristic model of initial system is derived according to spacecraft six-degree-of-freedom (6-DOF) dynamics. Correspondingly, by virtue of the low gain feedback technique, a characteristic model-based adaptive control strategy is developed, which can realize the attitude synchronization and position tracking in the presence of parameter uncertainties and bounded disturbances. Compared with the previous adaptive control design of spacecraft motion, the proposed control strategy possesses a simple structure, and can handle the actuator saturation and improve the robustness of the closed-loop system simultaneously. Numerical simulation indicates the validity of the control method.

Original languageEnglish
Title of host publicationProceedings of 2021 Chinese Intelligent Automation Conference
EditorsZhidong Deng
PublisherSpringer Science and Business Media Deutschland GmbH
Pages228-236
Number of pages9
ISBN (Print)9789811663710
DOIs
StatePublished - 2022
EventChinese Intelligent Automation Conference, CIAC 2021 - Zhanjiang, China
Duration: 5 Nov 20217 Nov 2021

Publication series

NameLecture Notes in Electrical Engineering
Volume801 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceChinese Intelligent Automation Conference, CIAC 2021
Country/TerritoryChina
CityZhanjiang
Period5/11/217/11/21

Keywords

  • Adaptive control
  • Characteristic model
  • Input saturation
  • Rendezvous and proximity operations

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