DocumentCode
1485243
Title
Analog computers in propeller control design
Author
Frick, R. K.
Author_Institution
Wright Air Development Center, Wright-Patterson Air Force Base, Ohio
Volume
76
Issue
10
fYear
1957
Firstpage
858
Lastpage
858
Abstract
IN THE PROCESS of designing and developing a dynamic system, provisions should be made for analysis of the performance of the system while it is still in the design stage. One method of analysis is to write the equations of motion of each moving part and then combine these equations in such a manner that a means of solution would be possible. This method is satisfactory if the system has few moving parts and, thereby, does not require many equations to describe its behavior. For a highly complex system, this will prove to be very laborious by longhand methods and should be submitted to machine computation for solution. The motion of the parts of the system may be such that an equation describing the behavior of any one part may be difficult to write unless approximations are made, and may have to be directly simulated by a device which has the proper dynamic characteristics built into it.
Keywords
Analog computers; Blades; Control systems; Engines; Equations; Mathematical model; Propellers;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1957.6442750
Filename
6442750
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