Finite-time-convergence Attitude Tracking Control for Rigid Spacecrafts Using Chebyshev ANN and Fast-NTSM Manifold-Reference-Cited by-同舟云学术

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Finite-time-convergence Attitude Tracking Control for Rigid Spacecrafts Using Chebyshev ANN and Fast-NTSM Manifold

Published:2022-06-27 Issue: Volume: Page:
ISSN:
Container-title:2022 IEEE 17th International Conference on Control & Automation (ICCA)
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Author:

Dimirovski Georgi M.¹,Jing Yuanwei²,Liu Xiaoping³

Affiliation:

1. SS Cyril & Methodius University in Skopje,Doctoral School FEIT

2. Northeastern University,College of Information Science & Engineering,Shenyang,Liaoning,P. R. China,110004

3. Lakehead University,Department of Electrical Engineering,Tunder Bay,ON,Canada,P7B 5E1

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9831427/9831807/09831913.pdf?arnumber=9831913

Reference46 articles.

1. Fixed-time control for high-precision attitude stabilization of flexible spacecraft

2. Finite-time tracking control of rigid spacecraft under actuator saturations and faults;xia;IEEE Transactions on Automation Science and Engineering,2016

3. Decentralized robust attitude tracking control for spacecraft networks under unknown inertia matrices

4. Adaptive Fuzzy Output Feedback Dynamic Surface Control of Interconnected Nonlinear Pure-Feedback Systems

5. Finite-time prescribed performance control for spacecraft attitude tracking;gao;IEEE/ASME Transactions on Mechatronics,2021

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