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Dynamic Modeling and Fully Actuated System Control for Liquid-Filled Spacecraft

  • Harbin Institute of Technology Shenzhen

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

Abstract

Dynamic modeling and controller design are investigated for attitude maneuvers of liquid-filled spacecraft within a fully actuated system framework. The controller design is based on a dynamical model of liquid-filled spacecraft derived from the theorem of angular momentum, where the liquid sloshing is equivalent to a spherical pendulum with three degrees of freedom. The attitude system of the dynamical model is cast into a fully actuated system expressed in error quaternions. Then, an observer-based adaptive controller is proposed to achieve attitude maneuvers of liquid-filled spacecraft with external disturbances. The controller consists of a general fully actuated system control law, a nonlinear disturbance observer, and an adaptive system. The control law provides a basic structure of the controller. The nonlinear disturbance observer estimates and compensates for the unknown perturbation consisting of external disturbances and liquid sloshing. The adaptive system deals with the estimated errors of the unknown perturbation and enhances the stability of the system. The stability of the controlled system is proved by Lyapunov’s direct method. Numerical simulations demonstrate the effectiveness of the proposed controller.

Original languageEnglish
Title of host publicationAdvances in Applied Nonlinear Dynamics, Vibration, and Control – 2024 - The Proceedings of 2024 International Conference on Applied Nonlinear Dynamics, Vibration and Control, ICANDVC 2024
EditorsXingjian Jing, Dixiong Yang, Hu Ding, Jiqiang Wang
PublisherSpringer Science and Business Media Deutschland GmbH
Pages494-508
Number of pages15
ISBN (Print)9789819633166
DOIs
StatePublished - 2025
Externally publishedYes
EventInternational Conference on Applied Nonlinear Dynamics, Vibration and Control, ICANDVC 2024 - Dalian, China
Duration: 25 Oct 202427 Oct 2024

Publication series

NameLecture Notes in Electrical Engineering
Volume1373 LNEE
ISSN (Print)1876-1100
ISSN (Electronic)1876-1119

Conference

ConferenceInternational Conference on Applied Nonlinear Dynamics, Vibration and Control, ICANDVC 2024
Country/TerritoryChina
CityDalian
Period25/10/2427/10/24

Keywords

  • Controller design
  • Dynamic modeling
  • Fully actuated system approach
  • Liquid-filled spacecraft

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