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.
Launcher attitude control: discrete-time robust design and gain-scheduling
Höhenregelung einer Startvorrichtung während des Flugs in der Erdatmosphäre: zeitdiskreter robuster Regelungsentwurf
Control Engineering Practice ; 11 , 11 ; 1243-1252
2003
10 Seiten, 12 Bilder, 19 Quellen
Article (Journal)
English
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