Global dynamics of a ring-tethered three-satellite system in any plane-Reference-Cited by-同舟云学术

Global dynamics of a ring-tethered three-satellite system in any plane

Published:2023-04-12 Issue:13 Volume:111 Page:11811-11821
ISSN:0924-090X
Container-title:Nonlinear Dynamics
language:en
Short-container-title:Nonlinear Dyn

Author:

Yu B. S.,Zhu Zheng H.^ORCID

Funder

Natural Science Foundation of Jilin Province

Natural Sciences and Engineering Research Council of Canada

Natural Science Foundation of Jiangsu Province

Aviation Science Foundation of China

Foundation of China Scholarship Council

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s11071-023-08451-5.pdf

Reference23 articles.

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3. Steindl, A.: Time optimal control for the deployment of a tethered satellite allowing for a massive tether. Meccanica 51(11), 2741–2751 (2016)

4. Lim, J., Chung, J.: Dynamic analysis of a tethered satellite system for space debris capture. Nonlinear Dyn. 94(4), 2391–2408 (2018)

5. Tarabini Castellani, L., Ortega, A., Giménez, A., Urgoiti, E., Sánchez-Arriaga, G., Borderes-Motta, G., Lorenzini, E.C., Tajmar, M., Wätzig, K., Post, A., Plaza, J.F.: Low work-function tether deorbit kit. J. Space Saf. Eng. 7(3), 332–339 (2020)

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