The current status of research on the application of variable structure system (VSS) theory to design aircraft flight control systems is summarized. Two aircraft types are currently being investigated: the Augmentor Wing Jet STOL Research Aircraft (AWJSRA), and AV-8A Harrier. The AWJSRA design considers automatic control of longitudinal dynamics during the landing phase. The main task for the AWJSRA is to design an automatic landing system that captures and tracks a localizer beam. The control task for the AV-8A is to track velocity commands in a hovering flight configuration. Much effort was devoted to developing computer programs that are needed to carry out VSS design in a multivariable frame work, and in becoming familiar with the dynamics and control problems associated with the aircraft types under investigation. Numerous VSS design schemes were explored, particularly for the AWJSRA. The approaches that appear best suited for these aircraft types are presented. Examples are given of the numerical results currently being generated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Application of Variable Structure System Theory to Aircraft Flight Control


    Beteiligte:
    A. J. Calise (Autor:in) / I. Kadushin (Autor:in) / F. Kramer (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Application of variable structure system theory to aircraft flight control

    Calise, A. J. / Kadushin, I. / Kramer, F. | NTRS | 1981


    Variable Camber Application to Aircraft in Formation Flight

    Liu, Yaolong / Stumpf, Eike | AIAA | 2016


    UNMANNED AIRCRAFT FLIGHT CONTROL APPLICATION AND UNMANNED AIRCRAFT FLIGHT CONTROL METHOD

    SUGAYA SHUNJI | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft flight control system

    BROT PATRICE | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT FLIGHT CONTROL SYSTEM

    TURUMKULOV MARAT TURAROVICH | Europäisches Patentamt | 2020

    Freier Zugriff