@inproceedings{e4e31d03badd4437bf1732b0188fb266,
title = "Approximate constrained time-optimal reorientation maneuvers using covariance matrix adaptation-evolutionary strategy",
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.",
author = "Melton, {Robert G.}",
year = "2014",
language = "English (US)",
series = "Advances in the Astronautical Sciences",
publisher = "Univelt Inc.",
pages = "1421--1433",
editor = "Mackison, {Donald L.} and Ossama Abdelkhalik and Wilson, {Roby S.} and Renato Zanetti",
booktitle = "Advances In The Astronautical Sciences",
address = "United States",
note = "24th AAS/AIAA Space Flight Mechanics Meeting, 2014 ; Conference date: 26-01-2014 Through 30-01-2014",
}