Method of forming a triangular rotating tethered constellation of spacecraft using electromagnetic forces

DOI10.1134/S1064230722040141MaRDI QIDQ2695146

Yu. M. Zabolotnov, Asiya A. Nazarova

Publication date: 30 March 2023

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Cites Work

• Three-dimensional multi-tethered satellite formation with the elements moving along Lissajous curves
• Control of the deployment of a tethered orbital system with a small load into a vertical position
• Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass
• Stabilizing the motion of a low-orbit electrodynamic tether system
• Unnamed Item

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