Distributed Finite-Time Attitude Tracking Control for Multiple Rigid Spacecrafts with Full-State Constraints-Reference-Cited by-同舟云学术

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Distributed Finite-Time Attitude Tracking Control for Multiple Rigid Spacecrafts with Full-State Constraints

Published:2024-05 Issue:3 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wang Songchen¹,Zhao Bin²^ORCID

Affiliation:

1. Graduate Student, Institute of Precision Guidance and Control, Northwestern Polytechnical Univ., Xi’an 710072, China.

2. Associate Professor, Institute of Precision Guidance and Control, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author). ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-5453

Reference26 articles.

1. Review of Formation Flying and Constellation Missions Using Nanosatellites

2. The leader-following attitude control of multiple rigid spacecraft systems

3. Review of attitude consensus of multiple spacecraft

4. Adaptive 2-bits-triggered neural control for uncertain nonlinear multi-agent systems with full state constraints

5. Attitude stabilization of rigid spacecraft with angular velocity and torque limitations

Cited by 1 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. Adaptive fuzzy ABLF function fixed‐time tracking control method for nonlinear fault‐tolerant control systems with event triggering mechanism;International Journal of Adaptive Control and Signal Processing;2024-07-22

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