DocumentCode :
1431387
Title :
The electronic servomechanism simulator
Author :
Edwards, G. M. ; Johnson, E. C.
Author_Institution :
Massachusetts Institute of Technology, Cambridge, Mass.
Volume :
69
Issue :
5
fYear :
1950
fDate :
5/1/1950 12:00:00 AM
Firstpage :
411
Lastpage :
411
Abstract :
A LARGE-SCALE analogue computer, capable of solving the general equations of motion of an aircraft, to be used primarily in the development of aircraft control systems is being developed at the Massachusetts Institute of Technology. The electronic servomechanism simulator is included as a portion of the computer to represent electrically the dynamic behavior of the servomechanisms which position the aircraft control surfaces. These servomechanisms usually are designed to operate linearly. However, a servomechanism which is small enough to be practical occasionally will be required to operate at the extreme limits of its physical capacity — beyond its linear range.
Keywords :
Aerospace control; Computational modeling; Damping; Limiting; Mathematical model; Servomechanisms; Torque;
fLanguage :
English
Journal_Title :
Electrical Engineering
Publisher :
ieee
ISSN :
0095-9197
Type :
jour
DOI :
10.1109/EE.1950.6433840
Filename :
6433840
Link To Document :
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