The application of system identification methods to high-bandwidth rotorcraft flight control system design is examined. Flight test and modeling requirements are illustrated using flight test data from a BO-105 hingeless rotor helicopter. The proposed approach involves the identification of nonparametric (transfer function and state space) model identification. Results for the BO-105 show the need for including coupled body/rotor flapping and lead-lag dynamics in the identification model structure to allow the accurate prediction of control ssytem bandwidth limitations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    System identification requirements for high-bandwidth rotorcraft flight control system design


    Beteiligte:

    Kongress:

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


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    System identification requirements for high-bandwidth rotorcraft flight control system design

    TISCHLER, MARK B. / U.S. Army / Aeroflightdynamics Directorate et al. | AIAA | 1990


    Flight requirements for operation of rotorcraft

    Scanlon, J. | Engineering Index Backfile | 1963



    ROTORCRAFT FLIGHT TRAINING METHOD, ASSOCIATED SYSTEM AND ROTORCRAFT

    DUMUR GUILLAUME / CHASSAGNE IVAN / OCKIER CARL | Europäisches Patentamt | 2024

    Freier Zugriff