Control of the deployment of a tethered orbital system with a small load into a vertical position
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Publication:2011414
DOI10.1016/J.JAPPMATHMECH.2015.04.015zbMath1432.70044OpenAlexW2020898173MaRDI QIDQ2011414
Publication date: 7 December 2019
Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jappmathmech.2015.04.015
Related Items (3)
Quasi-optimal stabilization of oscillatory systems with many degrees of freedom ⋮ Method of forming a triangular rotating tethered constellation of spacecraft using electromagnetic forces ⋮ Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass
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