TY - JOUR
T1 - Launcher attitude control
T2 - discrete-time robust design and gain-scheduling
AU - Voinot, Olivier
AU - Alazard, Daniel
AU - Apkarian, Pierre
AU - Mauffrey, Sophie
AU - Clément, Benoît
PY - 2003/11
Y1 - 2003/11
N2 - In this paper, a robust multi-objective design for the control of a launcher during atmospheric flight is investigated. This approach is based on the Cross Standard Form formulation which allows to incorporate the various specifications of the launcher problem in a streamlined manner. An important feature of this approach is that a non-conventional LQG/LTR approach, required to satisfy time-domain specifications, can be embedded into a more general standard problem in order to account for frequency-domain robustness constraints. The specific form of this standard problem is also very interesting for gain scheduling.
AB - In this paper, a robust multi-objective design for the control of a launcher during atmospheric flight is investigated. This approach is based on the Cross Standard Form formulation which allows to incorporate the various specifications of the launcher problem in a streamlined manner. An important feature of this approach is that a non-conventional LQG/LTR approach, required to satisfy time-domain specifications, can be embedded into a more general standard problem in order to account for frequency-domain robustness constraints. The specific form of this standard problem is also very interesting for gain scheduling.
KW - Cross standard form
KW - Gain scheduling
KW - Launcher
KW - Multi-objective design
KW - Robustness
UR - http://www.scopus.com/inward/record.url?scp=0142223962&partnerID=8YFLogxK
U2 - 10.1016/S0967-0661(02)00234-4
DO - 10.1016/S0967-0661(02)00234-4
M3 - Article
AN - SCOPUS:0142223962
VL - 11
SP - 1243
EP - 1252
JO - Control Engineering Practice
JF - Control Engineering Practice
SN - 0967-0661
IS - 11
ER -