DocumentCode
1370023
Title
Sinusoidal analysis of feedback-control systems containing nonlinear elements
Author
Johnson, E. Calvin
Author_Institution
Bendix Aviation Corporation, Detroit, Mich.
Volume
71
Issue
3
fYear
1952
fDate
7/1/1952 12:00:00 AM
Firstpage
169
Lastpage
181
Abstract
TECHNIQUES commonly used at the present time in the analysis and synthesis of feedback-control systems are largely those of constant-linear system theory. In the usual form, these methods stem from a system characterization in terms of ordinary linear differential equations having real constant coefficients. Fortunately, for many purposes this characterization is satisfactory, and in these cases the properties and behavior of the systems can be studied analytically by application of the large body of available linear theory. Frequently, however, practical control systems contain elements, either unavoidably or by design, which are not linear in the engineering sense of being describable by linear differential equations with constant coefficients.
Keywords
Aircraft; Circuit faults; Equations; Nonlinear systems; Oscillators; Steady-state; Transfer functions;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher
ieee
ISSN
0097-2185
Type
jour
DOI
10.1109/TAI.1952.6371220
Filename
6371220
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