DocumentCode :
853066
Title :
The Gyrovibrator
Author :
Diamantides, N.D.
Author_Institution :
Goodyear Aircraft Corp., Akron, Ohio
Issue :
1
fYear :
1959
fDate :
3/1/1959 12:00:00 AM
Firstpage :
16
Lastpage :
25
Abstract :
A new device for measuring angular rate is analyzed and its mechanical and electrical design features presented. Analytical proofs of three important characteristics of the instrument are given. These characteristics are: 1) a sinusoidally modulated-carrier voltage with the envelope representing the magnitude of the useful output signal; 2) zero drift as well as zero offset effects separated from the true output in the form of a dc quantity, and 3) a reference signal through which both the magnitude and the orientation of the input angular-velocity component in the plane of the spin are determined.
Keywords :
Aircraft; Computer displays; Gyroscopes; Human factors; Instruments; Military computing; Navigation; Testing; Velocity measurement; Vibration measurement;
fLanguage :
English
Journal_Title :
Aeronautical and Navigational Electronics, IRE Transactions on
Publisher :
ieee
ISSN :
0096-1639
Type :
jour
DOI :
10.1109/TANE3.1959.4201650
Filename :
4201650
Link To Document :
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