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Inverse optimal sliding mode control of spacecraft with coupled translation and attitude dynamics

  • Published:2015-02-13 Issue:13 Volume:46 Page:2421-2438
  • ISSN:0020-7721
  • Container-title:International Journal of Systems Science
  • language:en
  • Short-container-title:International Journal of Systems Science

Author:

Pukdeboon Chutiphon

Funder

King Mongkut's University of Technology North Bangkok and Thailand Research Fund (TRF)

Publisher

Informa UK Limited

Subject

Computer Science Applications,Theoretical Computer Science,Control and Systems Engineering

Cited by 25 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Spacecraft Close-range Attitude Tracking Control via Extended State Observer;2024 IEEE 7th Advanced Information Technology, Electronic and Automation Control Conference (IAEAC);2024-03-15

2. Coupled Dynamics and Integrated Control for Position and Attitude Motions of Spacecraft: A Survey;IEEE/CAA Journal of Automatica Sinica;2023-12

3. Coupled position and attitude control of a servicer spacecraft in rendezvous with an orbiting target;Scientific Reports;2023-03-14

4. H∞ inverse optimal attitude tracking on the special orthogonal group SO(3);International Journal of Control;2022-10-06

5. Adaptive Sliding Mode Control of a Perturbed Satellite in a Formation Antenna Array;IEEE Transactions on Aerospace and Electronic Systems;2022-10
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