Analytical guidance for spacecraft relative motion under constant thrust using relative orbit elements

Riccardo Bevilacqua, Thomas Alan Lovell

Research output: Contribution to journalArticlepeer-review

Original languageEnglish
Pages (from-to)47-61
Number of pages15
JournalActa Astronautica
Volume102
DOIs
StatePublished - 2014
Externally publishedYes

ASJC Scopus Subject Areas

  • Aerospace Engineering

Keywords

  • Analytical guidance
  • Input-shaping
  • On-off thrust
  • Relative orbit elements
  • Spacecraft relative motion

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