A method for designing fixed-gain controllers and filters for systems with large parameter variation is presented. The approach is based on finding the minimax point of the Kullback information measure between the fixed-gain system and the optimal system at a given operating point. The effectiveness of the proposed approach is illustrated by designing a fixed-gain system for the short-period control of a high-performance aircraft and evaluating its performance over the flight envelope.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Information Approach to Fixed-Gain Design


    Beteiligte:
    Baram, Yoram (Autor:in) / Eidelman, Doron (Autor:in)


    Erscheinungsdatum :

    01.01.1985


    Format / Umfang :

    1582620 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Information approach to fixed-gain design (aircraft control)

    Baram, Y. / Eidelman, D. | Tema Archiv | 1985


    Fixed Gain Controller Design for Aircraft

    Y. Baram / D. Eidelman | NTIS | 1981


    Gain-scheduling autopilot design based on fixed-structure synthesis

    Li, Bin / Lin, Defu / Wang, Hui et al. | IEEE | 2018


    Modern fixed structure control design. I - Gain adjustment to improve handling qualities

    Miotto, Piero / Paduano, James / Feron, Eric et al. | AIAA | 1997


    An Analytical Approach for Cislunar Information Gain

    Miga, Patrick | British Library Conference Proceedings | 2022