Velocity-Free Attitude Control for Flexible Spacecraft With Global Finite-Time Convergence-Reference-Cited by-同舟云学术

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Velocity-Free Attitude Control for Flexible Spacecraft With Global Finite-Time Convergence

Published:2024-09 Issue:9 Volume:71 Page:4226-4230
ISSN:1549-7747
Container-title:IEEE Transactions on Circuits and Systems II: Express Briefs
language:
Short-container-title:IEEE Trans. Circuits Syst. II

Author:

Zhu Wanwan¹^ORCID,Yang Yukai²^ORCID,Tian Bailing³^ORCID,Zong Qun³^ORCID

Affiliation:

1. School of Information and Control Engineering, China University of Mining and Technology, Xuzhou, China

2. Beijing Institute of Precision Mechatronics and Controls, Beijing, China

3. School of Electrical and Information Engineering, Tianjin University, Tianjin, China

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Link

http://xplorestaging.ieee.org/ielx7/8920/10666887/10478721.pdf?arnumber=10478721

Reference20 articles.

1. Fixed-Time Attitude Tracking Control for Rigid Spacecraft Without Angular Velocity Measurements

2. Adaptive Finite-Time 6-DOF Tracking Control for Spacecraft Fly Around With Input Saturation and State Constraints

3. Flexible Satellite Attitude Maneuver via Adaptive Sliding Mode Control and Active Vibration Suppression

4. Velocity-Free Attitude Reorientation of a Flexible Spacecraft with Attitude Constraints

5. Event-Triggered Policy to Spacecraft Attitude Stabilization With Actuator Output Nonlinearities

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