Optimal Sliding Guidance for Earth-Moon Halo orbit station-keeping and transfer

Joel Mueting, Roberto Furfaro, Francesco Topputo, Jules Simo

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

1 Scopus citations

Abstract

An Optimal Sliding Guidance (OSG) is implemented in the Circular Restricted Three-Body Problem and Restricted Four-Body Problem for spacecraft near libration points of the Earth-Moon system. Based on a combination of generalized Zero-Effort-Miss/Zero-Effort-Velocity and time-dependent sliding control theory, OSG is capable of generating closed-loop guided trajectories that are demonstrated to be globally finite-time stable against uncertain perturbing accelerations with known upper bound. The application of the OSG for Halo orbit station-keeping and orbital transfer are studied in a perturbed four body dynamical model in order to evaluate response and effectiveness of the proposed guidance approach.

Original languageEnglish (US)
Title of host publicationSpaceflight Mechanics 2016
PublisherUnivelt Inc.
Pages971-987
Number of pages17
Volume158
ISBN (Print)9780877036333
StatePublished - 2016
Event26th AAS/AIAA Space Flight Mechanics Meeting, 2016 - Napa, United States
Duration: Feb 14 2016Feb 18 2016

Other

Other26th AAS/AIAA Space Flight Mechanics Meeting, 2016
CountryUnited States
CityNapa
Period2/14/162/18/16

ASJC Scopus subject areas

  • Aerospace Engineering
  • Space and Planetary Science

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    Mueting, J., Furfaro, R., Topputo, F., & Simo, J. (2016). Optimal Sliding Guidance for Earth-Moon Halo orbit station-keeping and transfer. In Spaceflight Mechanics 2016 (Vol. 158, pp. 971-987). Univelt Inc..