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Attitude Maneuver Planning of Satellite for On-orbit Service with Spherical Geometric Constraints

  • School of Astronautics, Harbin Institute of Technology
  • China Aerospace Science and Technology Corporation

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

Abstract

In this paper, attitude maneuver planning problem of service satellite during on-orbit service (OOS) mission is addressed. Physical model is abstracted and problem of attitude maneuver planning path is extracted. A new attitude maneuver planning method with spherical geometric constraints is proposed to obtain the shortest and smooth attitude maneuver planning path when obstacles appeared between OOS system and target during maneuvering process. Simulation results can validate the effectiveness of the proposed approach.

Original languageEnglish
Title of host publicationProceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages513-518
Number of pages6
ISBN (Electronic)9781728137926
DOIs
StatePublished - Oct 2019
Externally publishedYes
Event2019 IEEE International Conference on Unmanned Systems, ICUS 2019 - Beijing, China
Duration: 17 Oct 201919 Oct 2019

Publication series

NameProceedings of the 2019 IEEE International Conference on Unmanned Systems, ICUS 2019

Conference

Conference2019 IEEE International Conference on Unmanned Systems, ICUS 2019
Country/TerritoryChina
CityBeijing
Period17/10/1919/10/19

Keywords

  • Attitude maneuver planning
  • OOS mission
  • obstacles
  • spherical geometric constraints

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