@inproceedings{e3f3e2dec0c1498a892aabcc11cda97a,
title = "Dynamics of the tethered space-tug system for the removal of geo defunct satellite",
abstract = "The tethered space-tug system is recognized as one of the most promising techniques to reduce the population of space debris. In this paper, the debris is specified as a large defunct GEO satellite equipped with one or two flexible appendages. A precise 3D dynamic model using Kane's method is derived. The dynamical behavior of the system is studied via numerical simulations, and some characteristics are revealed through this process.",
author = "Keying Yang and Shan Lu and Rui Qi and Yu Liu and Jingrui Zhang",
note = "Publisher Copyright: {\textcopyright} 2018 KASHYAP.; 4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 ; Conference date: 21-05-2018 Through 23-05-2018",
year = "2018",
language = "English",
isbn = "9780877036531",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "2037--2052",
editor = "Jeng-Shing Chern and Ya-Zhong Luo and Xiao-Qian Chen and Lei Chen",
booktitle = "Dynamics and Control of Space Systems",
address = "United States",
}