This paper describes a modeling method and a new optimal control approach to investigate a Mach number control problem for the NASA Ames 11-Foot Transonic Wind Tunnel. The flow in the wind tunnel is modeled by the 1-D unsteady Euler equations whose boundary conditions prescribe a controlling action by a compressor. The boundary control inputs to the compressor are in turn controlled by a drive motor system and an inlet guide vane system whose dynamics are modeled by ordinary differential equations. The resulting Euler equations are thus coupled to the ordinary differential equations via the boundary conditions. Optimality conditions are established by an adjoint method and are used to develop a model predictive linear-quadratic optimal control for regulating the Mach number due to a test model disturbance during a continuous pitch


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Adjoint Method and Predictive Control for 1-D Flow in NASA Ames 11-Foot Transonic Wind Tunnel


    Beteiligte:
    Nguyen, Nhan (Autor:in) / Ardema, Mark (Autor:in)

    Kongress:

    AIAA Aerospace Sciences Meeting and Exhibit ; 2006 ; Reno, NV, United States


    Erscheinungsdatum :

    01.01.2006


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    AIAA 2006-1433 Adjoint Method and Predictive Control for 1-D Flow in NASA Ames 11-Foot Transonic Wind Tunnel

    Nguyen, N. / Ardema, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006




    Calibration of the 11-By 11-Foot Transonic Wind Tunnel at the NASA Ames Research Center

    Amaya, M. A. / Boone, A. R. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2005