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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Information approach to fixed-gain design (aircraft control)


    Additional title:

    Verfahren fuer den Aufbau von Reglern mit fester Verstaerkung und Filtern mit grosser Parameteraenderung (Flugzeugleitung)


    Contributors:
    Baram, Y. (author) / Eidelman, D. (author)


    Publication date :

    1985


    Size :

    9 Seiten, 19 Quellen



    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Information Approach to Fixed-Gain Design

    Baram, Yoram / Eidelman, Doron | IEEE | 1985


    Fixed Gain Controller Design for Aircraft

    Y. Baram / D. Eidelman | NTIS | 1981


    Small unmanned fixed-wing aircraft design : a practical approach

    Keane, Andy J. / Sóbester, András / Scanlan, James P. | TIBKAT | 2017


    Flight Control System Design for Fixed Wing Aircraft

    Bodur, Aysenur / Ucun, Levent | IEEE | 2023


    Design and control for rotor-fixed wing hybrid aircraft

    Wang, Xinhua / Lin, Hai | SAGE Publications | 2011