@inproceedings{650c16cfcc244908b5fde89c2009951e,
title = "Multi-objective controller design for a space launcher",
abstract = "The design of an autopilot for a space launcher during the atmospheric stage is known to be a hard control problem, which contains an important number of conflicting specifications. This difficulty is increased by the presence of flexible modes, some of them acting inside the bandwidth, and parameter uncertainties.",
author = "M. Abbas-Turki and G. Duc and B. Clement",
year = "2007",
month = jul,
doi = "10.23919/ecc.2007.7068542",
language = "English",
series = "2007 European Control Conference, ECC 2007",
publisher = "Institute of Electrical and Electronics Engineers",
pages = "4016--4022",
booktitle = "2007 European Control Conference, ECC 2007",
address = "United States",
note = "2007 9th European Control Conference, ECC 2007 ; Conference date: 02-07-2007 Through 05-07-2007",
}