This paper describes an automatic flight control system in which the control surface follow-up element has been eliminated. In this system, the transfer characteristics of an electronic computer-amplifier are matched or made complementary to the transfer characteristics of a servo actuator in which the mechanical output is approximately the integral of an input electrical signal. This principle is in no way similar to that of a system in which the servo is simply a force generator and feedback is in the form of control surface reaction force.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Open Loop Flight Control System


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Younkin, J. R. (Autor:in)

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1968



    Erscheinungsdatum :

    03.04.1968




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Sensitivity of multiloop flight control system roots to open-loop parameter variations

    Stapleford, R.L. / McRuer, D.T. | Engineering Index Backfile | 1966


    Open-Loop Quadrotor Flight Dynamics Identification in Frequency Domain via Closed-Loop Flight Testing

    Niermeyer, Philipp / Raffler, Thomas / Holzapfel, Florian | AIAA | 2015


    Inner-Loop Flight Control

    Cai, Guowei / Chen, Ben M. / Lee, Tong Heng | Springer Verlag | 2011


    Open-Loop Stability of Flapping Flight in Hover

    Bolender, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010