A way for accelerated calculation of spacecraft motion in an atmosphere with a tethered aerodynamic stabilizer

DOI10.1134/S207004821401013XzbMath1356.70036OpenAlexW1976153492MaRDI QIDQ2961180

Yu. M. Zabolotnov, D. V. Elenev

Publication date: 17 February 2017

Published in: Mathematical Models and Computer Simulations (Search for Journal in Brave)

Full work available at URL: http://mathnet.ru/eng/mm3380

zbMATH Keywords

spacecrafttether systemaccelerated calculationaerodynamic stabilizerartificial increase of the oscillation periods

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20) Systems with slow and fast motions for nonlinear problems in mechanics (70K70)

Cites Work

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