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Application of singular perturbation theory to space flight dynamics problems

Danilo Zona Giulio Avanzini Fabrizio Giulietti Alessandro Palmas

航天动力学(英文)2025,Vol.9Issue(5):753-772,20.
航天动力学(英文)2025,Vol.9Issue(5):753-772,20.DOI:10.1007/s42064-024-0233-5

Application of singular perturbation theory to space flight dynamics problems

Application of singular perturbation theory to space flight dynamics problems

Danilo Zona 1Giulio Avanzini 1Fabrizio Giulietti 2Alessandro Palmas3

作者信息

  • 1. Department of Engineering for Innovation,University of Salento,Lecce 73100,Italy
  • 2. Department of Industrial Engineering,University of Bologna,Forlì campus 47121,Italy
  • 3. James Watt School of Engineering,University of Glasgow,Glasgow G12 8QQ,UK
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摘要

关键词

orbit decay/low-thrust trajectories/singular perturbation theory/two-timescale approximations

Key words

orbit decay/low-thrust trajectories/singular perturbation theory/two-timescale approximations

引用本文复制引用

Danilo Zona,Giulio Avanzini,Fabrizio Giulietti,Alessandro Palmas..Application of singular perturbation theory to space flight dynamics problems[J].航天动力学(英文),2025,9(5):753-772,20.

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