Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass

DOI10.3103/S0025654421070244OpenAlexW4200230137MaRDI QIDQ2070797

Ch. Wang, Yu. M. Zabolotnov

Publication date: 24 January 2022

Published in: Mechanics of Solids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3103/s0025654421070244

zbMATH Keywords

controlperturbationsdeploymentangular motion of nanosatellitesnanosatellitesorbital tether system

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (2)

Analysis of dynamics and control during the deployment of an annular tether group of spacecraft ⋮ Method of forming a triangular rotating tethered constellation of spacecraft using electromagnetic forces

Cites Work

• Unnamed Item
• Equilibrium configurations of the tethered three-body formation system and their nonlinear dynamics
• The effect of the elasticity of an orbital tether system on the oscillations of a satellite
• Dynamics of retrieval of a space tethered system
• Optimal control of deployment of a tethered subsatellite
• Control of the deployment of a tethered orbital system with a small load into a vertical position
• Resonant motions of the statically stable Lagrange spinning top
• The resonance motions of a statically stable Lagrange top at small nutation angles

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