DocumentCode :
817221
Title :
A numerical method for determining a system impulse response from the transient response to arbitrary inputs
Author :
Zabusky, N.
Author_Institution :
Hughes Aircraft Company, Los Angeles, CA, USA
Volume :
1
Issue :
1
fYear :
1956
fDate :
5/1/1956 12:00:00 AM
Firstpage :
40
Lastpage :
55
Abstract :
The transfer functions of large physical systems must be known if they are to be controlled efficiently. Environmental transient test procedures are described and their advantages presented. Because impulse and step functions cannot be obtained from practical test equipment, the problem of deducing the impulse response from arbitrary input and response data arises. A successful iteration procedure for determining h(\\tau ) , the impulse response, by using the convolution equation, r(t) = \\int_{o}^{\\infty} \\Theta (t-\\tau ) h (\\tau ) d\\tau , is described. An actual test transient is analyzed. An analog computer technique which mechanizes this iteration procedure is presented. The Appendix contains a tape multiplication procedure for performing numerical convolutions.
Keywords :
Aircraft manufacture; Aircraft propulsion; Analog computers; Frequency measurement; Predictive models; System testing; Transfer functions; Transient analysis; Transient response; Wind forecasting;
fLanguage :
English
Journal_Title :
Automatic Control, IRE Transactions on
Publisher :
ieee
ISSN :
0096-199X
Type :
jour
DOI :
10.1109/TAC.1956.1100811
Filename :
1100811
Link To Document :
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