Continuous thrust stationkeeping in earth-moon L1 halo orbits based on LQR control and floquet theory

Morad Nazari, William Anthony, Eric A. Butcher

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

Abstract

Three stationkeeping strategies in Earth-Moon L1 halo orbits are proposed based on continuous LQR control and Floquet theory using periodic control gains. The three strate- gies are based on time-periodic inffnite horizon LQR, backstepping technique with time- invariant LQR, and a dead-band periodic-gain controller. It is shown that the proposed controllers use less control effort than does traditional feedback linearization for the same settling time envelope of the tracking error.

Original languageEnglish (US)
Title of host publicationAIAA/AAS Astrodynamics Specialist Conference 2014
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624103087
DOIs
StatePublished - 2014
EventAIAA/AAS Astrodynamics Specialist Conference 2014 - San Diego, CA, United States
Duration: Aug 4 2014Aug 7 2014

Publication series

NameAIAA/AAS Astrodynamics Specialist Conference 2014

Other

OtherAIAA/AAS Astrodynamics Specialist Conference 2014
CountryUnited States
CitySan Diego, CA
Period8/4/148/7/14

ASJC Scopus subject areas

  • Aerospace Engineering
  • Astronomy and Astrophysics

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    Nazari, M., Anthony, W., & Butcher, E. A. (2014). Continuous thrust stationkeeping in earth-moon L1 halo orbits based on LQR control and floquet theory. In AIAA/AAS Astrodynamics Specialist Conference 2014 (AIAA/AAS Astrodynamics Specialist Conference 2014). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2014-4140