@inproceedings{f6876461c85e426f83d0b41ee628552a,
title = "Dynamics of the tethered geo defunct satellite with flexible appendages",
abstract = "There are many defunct satellites in geostationary orbit (GEO). The existence of them makes the GEO orbit crowded. And defunct satellites a potential source of great number of small space debris who poses a threat to the safety of wellworking satellites. By considering the vibration many destroy the flexible appendages of defunct satellites, this paper studied the dynamic of defunct satellites removal by space net. This paper simplifies the tug-tether-net-defunct satellite system into a TST system. The flexible panels are considered as thin plates with one fixed edge and three free edges. The TST system is analyzed, and the kinetic energy, gravitational potential energy, elastic potential energy and generalized force of system are obtained. The equations of motion of the formation are obtained by using Lagrange's equation.",
author = "Anrui Shi and Rui Qi and Shan Lu 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 = "2071--2078",
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",
}