A general technique for generating specifications for integrated flight propulsion control is extended to include systems with significant two-way coupling between the flight and propulsion systems. These specification define how the subsystems must perform within an integrated control system in order to assure that performance goals (specifically stability) are met when the subsystems are combined to form a closed-loop integrated system. Such specifications are useful for a large class of integrated control problems that are best approached in a partitioned or decentralized manner. An example demonstrating the application of these techniques to a simple helicopter problem is provided.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Integrated flight/propulsion control specifications for systems with two-way coupling


    Beteiligte:

    Kongress:

    1991 American Control Conference ; 1991 ; Boston, MA, United States


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Propulsion control specifications in integrated flight propulsion control systems

    ROCK, STEPHEN / EMAMI-NAEINI, ABBAS / ANEX, ROBERT | AIAA | 1988



    Integrated flight/propulsion control - Subsystem specifications

    Rock, Stephen M. / Ememi-Naeini, Abbas / Neighbors, Ken | AIAA | 1994



    Integrated Flight/Propulsion Control Specifications: Accounting for Two-Way Coupling

    Rock, S. / Neighbors, W. / AIAA | British Library Conference Proceedings | 1994