DocumentCode
1382241
Title
Hybrid digital analog pulse-time techniques for flight control system computers
Author
Seegmiller, W. R.
Author_Institution
General Electric Company, Schenectady, N. Y.
Volume
82
Issue
4
fYear
1963
Firstpage
498
Lastpage
503
Abstract
The application of hybrid digital analog pulse-time circuit techniques is presented in two specific examples for flight control system computers. These new circuit techniques make it practical to replace the electromechanical components, such as a-c servomotors, tachometers, synchros, and potentiometers, now used in flight control systems, with completely solidstate circuitry. This will result in increased reliability for flight control systems.
Keywords
Aerospace control; Aircraft; Flip-flops; Generators; Radiation detectors; Switching circuits; Synchronization;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part I: Communication and Electronics, Transactions of the
Publisher
ieee
ISSN
0097-2452
Type
jour
DOI
10.1109/TCE.1963.6373252
Filename
6373252
Link To Document