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contributor authorZhongjie Meng
contributor authorBingheng Wang
contributor authorPanfeng Huang
date accessioned2017-12-30T13:03:04Z
date available2017-12-30T13:03:04Z
date issued2017
identifier other%28ASCE%29AS.1943-5525.0000708.pdf
identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4245035
description abstractTowing spinning debris in space is subjected to the risk of twist, increasing the likelihood of collision. To reduce the twist potential, a twist suppression method is proposed for the viscoelastic tether in this paper. The system two-dimensional model is explored taking into account the attitude of the two end bodies and the tether slackness. The twist model describing the twist length is established to investigate the tension change during twist. The impedance based tension controller is designed to regulate tension actively by altering the tether unstretched length. Three cases where the thrust is 1 N, 2 N, and 5 N are studied to validate the feasibility of the method. It is shown that without tension control, towing removal is challenging for the system owing to the twist potential and large tension induced. However, the twist length is reduced dramatically and the relative distance of the two bodies is maintained under the tension control. It is also shown that the controller is robust to the measurement noise, and its performance is better for the lager thrust.
publisherAmerican Society of Civil Engineers
titleTwist Suppression Method of Tethered Towing for Spinning Space Debris
typeJournal Paper
journal volume30
journal issue4
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)AS.1943-5525.0000708
page04017012
treeJournal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 004
contenttypeFulltext


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