Exploiting distant periodic orbits and their invariant manifolds to design novel space trajectories to the Moon

Giorgio Mingotti, Francesco Topputo, Franco Bernelli-Zazzara

Research output: Chapter in Book/Report/Conference proceedingConference contribution book

4 Citations (Scopus)
Original languageEnglish
Title of host publicationSpaceflight Mechanics 2010
Subtitle of host publicationParts I-III
Place of PublicationUSA
Pages265-284
Volume136
Publication statusPublished - 14 Feb 2010
Event20th AAS/AIAA Space Flight Mechanics Meeting - San Diego, California
Duration: 14 Feb 201017 Feb 2010

Publication series

NameAdvances in the Astronautical Sciences
PublisherUnivelt Inc.
NumberI-III
Volume136
ISSN (Print)1081-6003

Conference

Conference20th AAS/AIAA Space Flight Mechanics Meeting
CitySan Diego, California
Period14/02/1017/02/10

Keywords

  • restricted three-body problem
  • low-thrust propulsion
  • mission design

Cite this

Mingotti, G., Topputo, F., & Bernelli-Zazzara, F. (2010). Exploiting distant periodic orbits and their invariant manifolds to design novel space trajectories to the Moon. In Spaceflight Mechanics 2010: Parts I-III (Vol. 136, pp. 265-284). (Advances in the Astronautical Sciences; Vol. 136, No. I-III). USA.