Dynamics of a flexible multi-tethered satellite formation in a halo orbit with uncertain parameters

DOI10.1016/J.CNSNS.2021.105828zbMath1477.70047OpenAlexW3137421307MaRDI QIDQ2025562

Caoqun Luo, Shidong Xu, Dongping Jin, Hao Wen

Publication date: 14 May 2021

Published in: Communications in Nonlinear Science and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cnsns.2021.105828

zbMATH Keywords

Chebyshev seriesinterval methoduncertain parametersmulti-tethered

Mathematics Subject Classification ID

Orthogonal polynomials and functions of hypergeometric type (Jacobi, Laguerre, Hermite, Askey scheme, etc.) (33C45) Orbital mechanics (70M20) Dynamical systems in classical and celestial mechanics (37N05)

Uses Software

• ode45

Cites Work

• Unnamed Item
• Nonlinear dynamic analysis of a three-body tethered satellite system with deployment/retrieval
• A Chebyshev interval method for nonlinear dynamic systems under uncertainty
• De-spinning of tethered space target via partially invariable deployment with tension control
• Attitude dynamics of three-body tethered systems
• Connecting orbits and invariant manifolds in the spatial restricted three-body problem

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