Deployment dynamics of tethered-net for space debris removal

Journal Article (2017)
Author(s)

Minghe Shan (TU Delft - Aerospace Engineering)

Jian Guo (TU Delft - Aerospace Engineering)

Eberhard Gill (TU Delft - Aerospace Engineering)

Research Group
Space Systems Egineering
DOI related publication
https://doi.org/10.1016/j.actaastro.2017.01.001 Final published version
More Info
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Publication Year
2017
Language
English
Research Group
Space Systems Egineering
Volume number
132
Pages (from-to)
293-302
Downloads counter
150

Abstract

A tethered-net is a promising method for space debris capturing. However, its deployment dynamics is complex because of the flexibility, and its dependency of the deployment parameters is insufficiently understood. To investigate the deployment dynamics of tethered-net, four critical deployment parameters, namely maximum net area, deployment time, traveling distance and effective period are identified in this paper, and the influence of initial deployment conditions on these four parameters is investigated. Besides, a comprehensive study on a model for the tethered-net based on absolute nodal coordinates formulation (ANCF) is provided. Simulations show that the results based on the ANCF modeling method present a good agreement with that based on the conventional mass–spring modeling method. Moreover, ANCF model is capable of describing the flexibility between two nodes on the net. However, it is more computationally expensive.