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
Link To Document :
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