DocumentCode :
487418
Title :
Experimental Identification of Modeling Errors in Dynamic Systems
Author :
Horak, Dan T.
Author_Institution :
Allied-Signal Aerospace Technology Center, 9140 Old Annapolis Road, Columbia, Maryland 21045
fYear :
1988
fDate :
15-17 June 1988
Firstpage :
1307
Lastpage :
1312
Abstract :
This paper presents a method for identifying the errors of a linear, time-invariant model of a dynamic system. The identification is based on system inputs and outputs recorded during an experiment. The identified errors are expressed as tolerances of the model parameters. These tolerances are such that a simulation of the dynamic system in which the linear model parameters are allowed to vary within their identified error tolerances can reproduce the response recorded during the experiment. The method is based on linear programming which guarantees that the identified errors are the smallest possible which can reproduce the experimental data. The model error information is useful for failure detection and isolation, system simulation and control design. The identification method is illustrated using a flight-dynamics example in conjunction with the Reachable Measurement Intervals (RMI) failure detection method for systems with modeling errors.
Keywords :
Aerodynamics; Condition monitoring; Control design; Equations; Error correction; Linear programming; Nonlinear dynamical systems; Parameter estimation; Size measurement; Time varying systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1988
Conference_Location :
Atlanta, Ga, USA
Type :
conf
Filename :
4789922
Link To Document :
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