A Method for designing fixed gain controllers and filters for systems with large parameter variation is presented. The approach, based of minmax information criteria, is used to design a non-adaptive back-up control system for a given aircraft and is shown to provide good performance qualities. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Fixed Gain Controller Design for Aircraft


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

    Publication date :

    1981


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Information approach to fixed-gain design (aircraft control)

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


    L1 Augmentations for a Fixed Gain Controller on a Large Transport Aircraft

    Wang, Mengmeng / Zhang, Shuguang / Holzapfel, Florian et al. | AIAA | 2017




    A coordinated turn controller for a fixed-wing aircraft

    Corona-Sánchez, José J / Guzmán Caso, Óscar Roberto / Rodríguez-Cortés, H | SAGE Publications | 2019