Non-Singular Fast Terminal Sliding Mode Control with Super-Twisting ESO for Spacecraft Formation Flying Systems-Reference-Cited by-同舟云学术

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Non-Singular Fast Terminal Sliding Mode Control with Super-Twisting ESO for Spacecraft Formation Flying Systems

Published:2023-11-17 Issue: Volume: Page:6866-6871
ISSN:
Container-title:2023 China Automation Congress (CAC)
language:
Short-container-title:

Author:

Li Yufei¹,Tang Feilong²,Zhong Xiaoqing³,Xiang Zhihua²,Ju Yinhao²,Huan Baizheng²

Affiliation:

1. School of Aerospace Engineering, Beijing Institute of Technology,Beijing,China

2. Harbin Institute of Technology,Department of Control Science and Engineering,Harbin,China

3. Institute of Telecommunication Satellite,China Academy of Space Technology,Beijing,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10450150/10449968/10451788.pdf?arnumber=10451788

Reference17 articles.

1. Invariant relative orbits for spacecraft formation flying in high-order gravitational field

2. Spacecraft formation flying system design and controls for four nanosats mission

3. Perturbed State-Transition Matrix for Spacecraft Formation Flying Terminal-Point Guidance

4. The gravity recovery and climate experiment: Mission overview and early results

5. TechSat 21: formation design, control, and simulation

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