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Finite-time Velocity-free Attitude-orbit Integrated Tracking Control for Rigid Spacecraft

  • Harbin Institute of Technology
  • Beijing Institute of Tracking and Communication Technology

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

Abstract

In this paper, an attitude-orbit integrated controller is designed for rigid spacecraft without velocity and angular velocity measurement. First, based on dual quaternion description, the integrated attitude-orbit kinematics and dynamics model for rigid spacecraft is presented. On this basis, an attitude-orbit integrated output feedback control strategy is developed in the absence of velocity information, and the finite-time convergence of the control system is analyzed. Finally, the numerical simulation is given to verify the effectiveness and feasibility of the proposed velocity-free control strategy.

Original languageEnglish
Title of host publication2022 8th International Conference on Control, Automation and Robotics, ICCAR 2022
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages357-362
Number of pages6
ISBN (Electronic)9781665481168
DOIs
StatePublished - 2022
Event8th International Conference on Control, Automation and Robotics, ICCAR 2022 - Xiamen, China
Duration: 8 Apr 202210 Apr 2022

Publication series

Name2022 8th International Conference on Control, Automation and Robotics, ICCAR 2022

Conference

Conference8th International Conference on Control, Automation and Robotics, ICCAR 2022
Country/TerritoryChina
CityXiamen
Period8/04/2210/04/22

Keywords

  • Dual quaternion
  • attitude-orbit integrated control
  • finite-time control
  • output feedback control
  • velocity-free control

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