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Rotation matrix-based finite-time attitude coordinated control for spacecraft

  • Published:2022-01 Issue:2 Volume:69 Page:976-988
  • ISSN:0273-1177
  • Container-title:Advances in Space Research
  • language:en
  • Short-container-title:Advances in Space Research

Author:

Tan Chao,Xu Guodong,Dong Limin,Xie Yaen,He Yushan,Hao Yong,Han Fei

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Cited by 8 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. Unwinding-Free Attitude Control via Fully Actuated System Approach;2024 3rd Conference on Fully Actuated System Theory and Applications (FASTA);2024-05-10

2. Adaptive super-twisting sliding mode attitude coordination control for spacecraft formation flying with actuator saturation;Advances in Space Research;2023-11

3. Fault-tolerant attitude coordination control for multiple flexible spacecraft using vector measurements;Advances in Space Research;2023-09

4. Research on Finite-Time Sliding Mode Control Algorithm for Vehicle System;Dynamical Systems and Control;2023

5. Literature Review;Distributed Attitude Consensus of Multiple Flexible Spacecraft;2022-09-18
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