The problems of design criteria and architecture of multiloop flight control systems 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 are discussed. Joint root locus and quality criteria design are presented. The structure of the presented multiloop flight control system consists of nonlinear open loop control for flight performance and flight management; superposed quasilinear state vector feedback; and six control surfaces (aileron, rudder, elevator, trim, throttle, direct lift/drag control).


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    Titel :

    Design Criteria for Multi-Loop Flight Control Systems


    Beteiligte:
    G. Schaenzer (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Design Criteria for Optimal Flight Control Systems

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


    Design criteria for optimal flight control systems

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