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.


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    Titel :

    Launcher attitude control: discrete-time robust design and gain-scheduling


    Weitere Titelangaben:

    Höhenregelung einer Startvorrichtung während des Flugs in der Erdatmosphäre: zeitdiskreter robuster Regelungsentwurf


    Beteiligte:
    Voinot, O. (Autor:in) / Alazard, D. (Autor:in) / Apkarian, P. (Autor:in) / Mauffrey, S. (Autor:in) / Clement, B. (Autor:in)

    Erschienen in:

    Control Engineering Practice ; 11 , 11 ; 1243-1252


    Erscheinungsdatum :

    2003


    Format / Umfang :

    10 Seiten, 12 Bilder, 19 Quellen




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Robust Trajectory and Attitude Control of a Flexible Launcher

    Bernelli-Zazzera, F. / European Space Agency | British Library Conference Proceedings | 2003


    A Robust Multi-Objective Synthesis Applied to Launcher Attitude Control

    Voinot, O. / Alazard, D. / Piquereau, A. et al. | British Library Conference Proceedings | 2002


    Robust Analysis of a Launcher Attitude Controller via mu-Analysis

    Imbert, N. / International Federation of Automatic Control | British Library Conference Proceedings | 2002


    Gain Scheduling for an Aerospace Launcher with Bending Modes

    Clement, B. / Duc, G. / Mauffrey, S. et al. | British Library Conference Proceedings | 2002


    Embedding FDI in launcher attitude controllers

    Ramos, Fausto / Alazard, Daniel | IEEE | 2009