The operation of a control surface actuator and its steady state valve characteristics are examined. The linearized transfer functions are calculated under simplified assumptions. Suitable parameters are defined and their influence on the stability of the closed loop is discussed. The response of the closed position control loop is demonstrated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Dynamic Response of a Hot Gas, Control-Surface Actuator


    Beteiligte:
    E. Goellner (Autor:in)

    Erscheinungsdatum :

    1981


    Format / Umfang :

    72 pages



    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Dynamic Identification of Actuator Frequency Response

    Bachelder, Edward / Klyde, David / Lee, Dongchan et al. | AIAA | 2007


    AIRCRAFT CONTROL SURFACE ACTUATOR

    DAVIES JONATHAN | Europäisches Patentamt | 2019

    Freier Zugriff

    Dynamic Identification of Actuator Frequency Response AIAA Paper

    Bachelder, E. / Klyde, D. / Millar, R. et al. | British Library Conference Proceedings | 2007


    Dynamic surface attack angle control for aircraft considering actuator position saturation

    Liu, Xiaodong / Sheng Sun, / Pengjie Lan, et al. | IEEE | 2016


    Actuator for flight control surface

    GOMOLKO OLEG / MERLET ETIENNE | Europäisches Patentamt | 2018

    Freier Zugriff