Prescribed-time attitude control during solid thrusting orbital maneuver

Junjie Lu, Zhongjie Meng

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

2 Scopus citations

Abstract

With the development of aerospace technology, solid propulsion system is gradually applied in the orbital maneuver missions. However, there are some unavoidable problems of solid thruster, such as the strong time constraint caused by the fuel limitation and the strong unknown attitude disturbance caused by the thrust misalignment. In this paper, a prescribed-time attitude stabilization control strategy based on thrust vector control (TVC) technique is proposed. Firstly, the attitude dynamics model of the solid propulsion satellite is established. Considering the strictly limited control time during orbital maneuver, the time-varying constraint boundary function is constructed based on the prescribed time and attitude accuracy requirements. Then, the prescribed-time attitude controller is designed on the basis of the adaptive backstepping method, and the prescribed-time stability of the satellite system is proved via Lyapunov stability theory. Finally, simulations verify the effectiveness of the proposed prescribed-time controller for attitude control of the satellite during solid thrusting orbital maneuver.

Original languageEnglish
Title of host publicationICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications
EditorsWenxiang Xie, Shibin Gao, Xiaoqiong He, Xing Zhu, Jingjing Huang, Weirong Chen, Lei Ma, Haiyan Shu, Wenping Cao, Lijun Jiang, Zeliang Shu
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages58-63
Number of pages6
ISBN (Electronic)9781665409841
DOIs
StatePublished - 2022
Event17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022 - Chengdu, China
Duration: 16 Dec 202219 Dec 2022

Publication series

NameICIEA 2022 - Proceedings of the 17th IEEE Conference on Industrial Electronics and Applications

Conference

Conference17th IEEE Conference on Industrial Electronics and Applications, ICIEA 2022
Country/TerritoryChina
CityChengdu
Period16/12/2219/12/22

Keywords

  • Constraint boundary function
  • Orbital maneuver
  • Prescribed-time control
  • Solid thruster
  • Thrust vector control

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