Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval
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Publication:330736
DOI10.1007/S11071-015-2221-ZzbMath1441.70013OpenAlexW839821639WikidataQ57435628 ScholiaQ57435628MaRDI QIDQ330736
Andre P. Mazzoleni, Wonyoung Jung, Jintai Chung
Publication date: 26 October 2016
Published in: Nonlinear Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s11071-015-2221-z
deployment and retrievallibration anglenonlinear dynamic behaviorthree-body tethered satellite system
Related Items (4)
An analytical control law of length rate for tethered satellite system ⋮ Vibration and elastic wave propagation in spatial flexible damping panel attached to four special springs ⋮ Dynamics of a flexible multi-tethered satellite formation in a halo orbit with uncertain parameters ⋮ Optimal deployment of spin-stabilized tethered formations with continuous thrusters
Cites Work
- Equilibrium configurations of the tethered three-body formation system and their nonlinear dynamics
- Optimal feedback control of the deployment of a tethered subsatellite subject to perturbations
- Some properties of the dumbbell satellite attitude dynamics
- Advances in dynamics and control of tethered satellite systems
- Attitude dynamics of three-body tethered systems
- General formulation for N-body tethered satellite system dynamics
- Dumbbell librations in elliptic orbits
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