Approximate constrained time-optimal reorientation maneuvers using covariance matrix adaptation-evolutionary strategy

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

Abstract

The CMA-ES method is applied directly to the constrained satellite reorientation problem. This method is shown to give a very good approximate optimal solution to the constrained problem. The paper examines the performance for the constrained problem, and considers a modification that removes the eigendecomposition step in the early stages of the iteration to achieve greater computational speed.

Original languageEnglish (US)
Title of host publicationAdvances In The Astronautical Sciences
EditorsDonald L. Mackison, Ossama Abdelkhalik, Roby S. Wilson, Renato Zanetti
PublisherUnivelt Inc.
Pages1421-1433
Number of pages13
ISBN (Electronic)9780877036111
StatePublished - Jan 1 2014
Event24th AAS/AIAA Space Flight Mechanics Meeting, 2014 - Mexico, United States
Duration: Jan 26 2014Jan 30 2014

Publication series

NameAdvances in the Astronautical Sciences
Volume152
ISSN (Print)0065-3438

Other

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

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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