@inproceedings{4802ce009c5442e5907419cd74547f9b,
title = "Optimal Sliding Guidance for Earth-Moon Halo orbit station-keeping and transfer",
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.",
author = "Joel Mueting and Roberto Furfaro and Francesco Topputo and Jules Simo",
year = "2016",
language = "English (US)",
isbn = "9780877036333",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "971--987",
editor = "Ozimek, {Martin T.} and Renato Zanetti and Bowes, {Angela L.} and Russell, {Ryan P.} and Ozimek, {Martin T.}",
booktitle = "Spaceflight Mechanics 2016",
note = "26th AAS/AIAA Space Flight Mechanics Meeting, 2016 ; Conference date: 14-02-2016 Through 18-02-2016",
}