The problems of design criteria and architecture of multiloop flight control systems are discussed for a realized system to achieve precise flight path guidance, safe and economic control of the aerodynamic flow (airspeed, angle of attack and lift coefficient control) and passenger comfort. Joint root locus and quality criteria design presented. The structure of the presented multiloop flight control system consists of nonlinear open loop control for flight performance and flight management purpose, superposed quasi linear state vector feed back and six control surfaces (aileron, rudder, elevator, trim, throttle, direct lift/drag control).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design Criteria Multi-Loop Flight Control Systems


    Beteiligte:
    G. Schsenzer (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Design Criteria for High-Authority Closed-Loop Primary Flight Control Systems

    R. C. Hendrick / A. J. Bailey / L. D. Edinger et al. | NTIS | 1972


    Design criteria for optimal flight control systems

    GOVINDARAJ, K. / RYNASKI, E. | AIAA | 1979


    Design Criteria for Optimal Flight Control Systems

    K.S. Govindaraj / E.G. Rynaski | AIAA | 1980