Equilibrium configurations of the tethered three-body formation system and their nonlinear dynamics
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Publication:315446
DOI10.1007/S10409-012-0160-1zbMath1345.70014OpenAlexW2039894087MaRDI QIDQ315446
Jian-Min Zhu, Tian Tan, Ming Xu, Shi-Jie Xu
Publication date: 21 September 2016
Published in: Acta Mechanica Sinica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s10409-012-0160-1
equilibrium configurationformation flyinghomoclinic/heteroclinic connectionLyapunov orbittethered satellites system
Three-body problems (70F07) Homoclinic and heteroclinic trajectories for nonlinear problems in mechanics (70K44)
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Exact mesh shape design of large cable-network antenna reflectors with flexible ring truss supports ⋮ Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval ⋮ Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass
Cites Work
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- \(J _{2}\) invariant relative orbits via differential correction algorithm
- Nonlinear dynamical analysis for displaced orbits above a planet
- Attitude dynamics of three-body tethered systems
- Dynamics and Mission Design Near Libration Points
- Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
- General formulation for N-body tethered satellite system dynamics
- E/I-vector separation for safe switching of the GRACE formation
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