@inproceedings{b22d371aedc644728e746ff19b15a0f9,
title = "Time optimal control of a satellite with two rotors",
abstract = "The aim of this work is to investigate the structure of time-optimal trajectories for a control system modelizing a satellite with two rotors attached along its two fixed axes. Our results extend to the general case those obtained by Sussmann and Tang in an unpublished paper where they treat a particular case described below. We end up finding a sufficient family of four parameters trajectory types. The main tools used are the Pontryagin Maximum Principle, switching functions and envelope theory.",
author = "U. Boscain and Y. Chitour and B. Piccoli",
note = "Publisher Copyright: {\textcopyright} 2001 EUCA.; 6th European Control Conference, ECC 2001 ; Conference date: 04-09-2001 Through 07-09-2001",
year = "2001",
doi = "10.23919/ecc.2001.7076169",
language = "English (US)",
series = "2001 European Control Conference, ECC 2001",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1721--1725",
booktitle = "2001 European Control Conference, ECC 2001",
address = "United States",
}