DocumentCode
343195
Title
Control of the NASA Langley 16-foot transonic tunnel with the self-organizing map
Author
Motter, Mark A.
Author_Institution
Flight Dynamics & Control Div., NASA Langley Res. Center, Hampton, VA, USA
Volume
3
fYear
1999
fDate
1999
Firstpage
1659
Abstract
A predictive, multiple model control strategy is developed based on an ensemble of local linear models of the nonlinear system dynamics for a transonic wind tunnel. The local linear models are estimated directly from the weights of a self-organizing map (SOM). Multiple self-organizing maps collectively model the global response of the wind tunnel to a finite set of representative prototype controls. These prototype controls partition the control space and incorporate experiential knowledge gained from decades of operation. Each SOM models the combination of the tunnel with one of the representative controls, over the entire range of operation. The SOM based linear models are used to predict the tunnel response to a larger family of control sequences which are on the representative prototypes. The control which corresponds to the prediction that best satisfies the requirements on the system output is applied as the external driving signal. Each SOM provides a codebook representation of the tunnel dynamics corresponding to a prototype control. Different dynamic regimes are organized into topological neighborhoods where the adjacent entries in the codebook represent the minimization of a similarity metric which is the essence of the self organizing feature of the map. Thus, the SOM is additionally employed to identify the local dynamical regime, and consequently implements a switching scheme that selects the best available model for the applied control. Experimental results of controlling the wind tunnel, with the proposed method, during operational runs where strict research requirements on the control of the Mach number were met, are presented
Keywords
aerodynamics; neurocontrollers; self-organising feature maps; wind tunnels; Mach number; NASA Langley 16-foot transonic tunnel; control sequences; global response; local linear models; predictive multiple model control strategy; prototype controls; self-organizing map; topological neighborhoods; tunnel dynamics; Control systems; NASA; Nonlinear control systems; Nonlinear dynamical systems; Nonlinear systems; Predictive models; Prototypes; Self organizing feature maps; Signal processing; Wind forecasting;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1999. Proceedings of the 1999
Conference_Location
San Diego, CA
ISSN
0743-1619
Print_ISBN
0-7803-4990-3
Type
conf
DOI
10.1109/ACC.1999.786111
Filename
786111
Link To Document