Sliding-mode control system for the three-axis attitude control of rigid-body spacecraft with unknown dynamics parameters-Reference-Cited by-同舟云学术

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Sliding-mode control system for the three-axis attitude control of rigid-body spacecraft with unknown dynamics parameters

Published:1991-10 Issue:4 Volume:54 Page:737-761
ISSN:0020-7179
Container-title:International Journal of Control
language:en
Short-container-title:International Journal of Control

Author:

DODDS S. J.,WALKER A. B.

Publisher

Informa UK Limited

Subject

Computer Science Applications,Control and Systems Engineering

Link

http://www.tandfonline.com/doi/pdf/10.1080/00207179108934184

Reference7 articles.

1. Continuous approximation of variable structure control

2. MEYER , G. , 1966 , On the use of Euler's theorem on rotations for the synthesis of attitude control systems . NASA TN D-3643 .

Cited by 7 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. Robust attitude tracking control of spacecraft under unified actuator dynamics;International Journal of Control;2022-03-30

2. Anti-Unwinding Sliding Mode Attitude Maneuver Control for Rigid Spacecraft;IEEE Transactions on Automatic Control;2022-02

3. Sliding mode control of photoelectric tracking platform based on the inverse system method;MATEC Web of Conferences;2016

4. Finite-time attitude tracking control for a rigid spacecraft using time-varying terminal sliding mode techniques;International Journal of Control;2015-01-09

5. High-Precision Attitude Control of Remote Sensing Satellite;IFAC Proceedings Volumes;2004-06

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