Two Approaches to Optimal Sensor Locations

Author:

Fadale T. D.1,Nenarokomov A. V.2,Emery A. F.3

Affiliation:

1. Department of Aeronautics and Astronautics, University of Washington, Seattle, WA 98185

2. Department of Space System Engineering, Moscow Aviation Institute, Moscow, Russia

3. Department of Mechanical Engineering, University of Washington, Seattle, WA 98185

Abstract

Accurate modeling of thermal systems depends upon the determination of the material properties and the surface heat transfer coefficients. These parameters are frequently estimated from temperatures measured within the system or on the surface or from measured surface heat fluxes. Because of sensor errors or lack of sensitivity, the measurements may lead to erroneous estimates of the parameters. These errors can be ameliorated if the sensors are placed at points of maximum sensitivity. This paper describes two methods to optimize sensor locations: one to account for signal error, the other to consider interacting parameters. The methods are based upon variants of the normalized Fisher information matrix and are shown to be equivalent in some cases, but to predict differing sensor locations under other conditions, usually transient.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference25 articles.

1. Artyukhin E. A. , 1985, “Experimental Design of Measurement of the Solution of Coefficient-Type Inverse Heat Conduction Problem,” Journal of Engineering Physics, Vol. 48, No. 3, pp. 372–376.

2. Artyukhin E. A. , and NenarokomovA. V., 1988, “Optimal Experimental Design for Determining the Total Emissivity of Materials,” High Temperatures, Vol. 26, No. 5, pp. 761–767.

3. Beck, J. V., and Arnold, K. J., 1977, Parameter Estimation in Engineering and Science, Wiley, New York.

4. Beck, J. V., et al., 1992, “Joint American-Russian NSF Workshop on Inverse Problems in Heat Transfer,” Michigan State University.

5. Cruse, T. A., 1989, “Probabilistic Structural Analysis Methods (PSAM) for Select Space Propulsion Components,” manuscript prepared under SwRI Project No. 06-8338, NASA Contract NAS3-24389.

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