Near optimal feedback guidance design and the planar restricted three-body problem

Joseph Dinius, Roberto Furfaro, Francesco Topputo, Scott Selnick

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

Abstract

In this paper, we present the application of the ZEM/ZEV guidance algorithm to the planar restricted three-body problem (PR3BP). The ZEM/ZEV guidance law as a feedback guidance strategy is presented and applied to the PR3BP. The fuel optimal solution to the PR3BP for a transfer from GTO to L<inf>1</inf> in the Earth-Moon system is presented as a point for comparison, showing the near optimality of the closed-loop guidance approach. Challenges of the approach and strategies for implementation in spacecraft mission design are discussed.

Original languageEnglish (US)
Title of host publicationAdvances in the Astronautical Sciences
PublisherUnivelt Inc.
Pages575-584
Number of pages10
Volume152
ISBN (Print)9780877036111
StatePublished - 2014
Event24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States
Duration: Jan 26 2014Jan 30 2014

Other

Other24th AAS/AIAA Space Flight Mechanics Meeting, 2014
Country/TerritoryUnited States
CityMexico
Period1/26/141/30/14

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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