Attainable sets in space mission design: A method to define low-thrust, invariant manifold trajectories

Giorgio Mingotti, Francesco Topputo, Franco Bernelli-Zazzara

Research output: Chapter in Book/Report/Conference proceedingChapter

1 Citation (Scopus)
Original languageEnglish
Title of host publicationSpaceflight Mechanics 2012
Pages541-556
Volume143
ISBN (Electronic)978-0-87703-581-7
Publication statusPublished - Feb 2012
Event22nd AAS/AIAA Spaceflight Mechanics Meeting - Charleston, South Carolina, United States
Duration: 29 Jan 20122 Feb 2012

Publication series

NameAdvances in the Astronautical Sciences
PublisherUnivelt Inc
Number1-3
Volume143
ISSN (Print)1081-6003

Conference

Conference22nd AAS/AIAA Spaceflight Mechanics Meeting
CountryUnited States
CityCharleston, South Carolina
Period29/01/122/02/12

Keywords

  • restricted 3-body problem
  • Earth-Moon trajectories
  • low-energy
  • periodic orbits
  • transit orbits
  • transfers
  • optimisation
  • capture
  • system
  • Mars

Cite this

Mingotti, G., Topputo, F., & Bernelli-Zazzara, F. (2012). Attainable sets in space mission design: A method to define low-thrust, invariant manifold trajectories. In Spaceflight Mechanics 2012 (Vol. 143, pp. 541-556). (Advances in the Astronautical Sciences; Vol. 143, No. 1-3).