DocumentCode
858156
Title
Nongyroscopic inertial reference
Author
Klein, J.J.
Author_Institution
Lockheed Aircraft Corp., Sunnyvale, CA, USA
Volume
4
Issue
2
fYear
1959
fDate
11/1/1959 12:00:00 AM
Firstpage
182
Lastpage
191
Abstract
The space stabilizing capability of a servo controlled nonrotating inertial mass is analyzed and its drift rate performance compared with a high precision gyroscope. The results indicate that the nongyroscopic inertial reference and guidance system exceeds the performance of gyroscopic systems by several orders of magnitude. It is shown that a servo system materially contributes to the drift accuracy in the nongyroscopic system but not in the gyroscopic system. The navigation errors of the discussed scheme are directly proportional to the accelerometer errors and, therefore, are inherently smaller than in an equivalent gyroscopic system.
Keywords
Accelerometers; Containers; Glass; Gyroscopes; Missiles; Navigation; Servomechanisms; Torque control; Weight control; Wheels;
fLanguage
English
Journal_Title
Automatic Control, IRE Transactions on
Publisher
ieee
ISSN
0096-199X
Type
jour
DOI
10.1109/TAC.1959.1104858
Filename
1104858
Link To Document