Design and optimization of low-thrust orbit transfers

Seungwon Lee, Paul Von Allmen, Wolfgang Fink, Anastassios E. Petropoulos, Richard J. Terrile

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

26 Scopus citations

Abstract

NASA's space missions Dawn and JIMO will use low-thrust propulsion for multi-revolution orbit transfers around a central body. Here we address the problem of designing low-thrust orbit transfers between arbitrary orbits in an inverse-square gravity field by using evolutionary algorithms to drive parameter selection in a Lyapunov feedback control law (the Q-law). We develop an efficient and efficacious method to assess, with reasonable accuracy, the trade off between propellant mass and flight time (i.e., to find the Pareto front for these two quantities), and to provide the time history of the state variables and the thrust vector for any chosen point on the Pareto front.

Original languageEnglish (US)
Title of host publicationProceedings - 2005 IEEE Aerospace Conference
PublisherIEEE Computer Society
Pages855-869
Number of pages15
ISBN (Print)0780388704, 9780780388703
DOIs
StatePublished - 2005
Event2005 IEEE Aerospace Conference - Big Sky, MT, United States
Duration: Mar 5 2005Mar 12 2005

Publication series

NameIEEE Aerospace Conference Proceedings
Volume2005
ISSN (Print)1095-323X

Other

Other2005 IEEE Aerospace Conference
CountryUnited States
CityBig Sky, MT
Period3/5/053/12/05

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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    Lee, S., Von Allmen, P., Fink, W., Petropoulos, A. E., & Terrile, R. J. (2005). Design and optimization of low-thrust orbit transfers. In Proceedings - 2005 IEEE Aerospace Conference (pp. 855-869). [1559377] (IEEE Aerospace Conference Proceedings; Vol. 2005). IEEE Computer Society. https://doi.org/10.1109/AERO.2005.1559377