DocumentCode
1146293
Title
Minitact gyroscope-the low cost alternative
Author
Califano, Herbert T.
Author_Institution
AlliedSignal Guidance & Control System, Teterboro, NJ, USA
Volume
9
Issue
8
fYear
1994
Firstpage
12
Lastpage
16
Abstract
The allure of the solid state optical gyros is being challenged by the invention of a new spinning mass device, providing superior low noise drift performance, high reliability at a very low cost. The Minitact is a unique two axis gyroscope advancing the technology of spinning mass devices to set new low cost standards. Minitact provides all the low noise performance benefits of tuned rotor gyroscopes without the vagaries of fixture suspension systems. The Minitact design integrates together the advantages of a spherical hydrodynamic gas bearing and a three axis permanent magnet DC commutated, motor and torquer, into miniature two aids gyroscope with a dynamic range of greater than 10/sup -7/. The design is described and performance data presented illustrating the capability of this low cost next generation rate gyroscope. The Minitact is the result of Integrated Product Development (IPD) and Design to Unit Production Cost (DTUPC) design processes and is expected to become the tactical performance benchmark.<>
Keywords
gyroscopes; military equipment; navigation; permanent magnet motors; Design to Unit Production Cost; Integrated Product Development; Minitact gyroscope; cost; design; mechanical gyro; military equipment; navigation; noise drift performance; permanent magnet DC motor; reliability; spherical hydrodynamic gas bearing; spinning mass device; spinning mass devices; standards; tactical performance benchmark; tuned rotor gyroscopes; two axis gyroscope; Costs; Fixtures; Gyroscopes; Hydrodynamics; Magnetic levitation; Optical devices; Optical noise; Rotors; Solid state circuits; Spinning;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/62.311238
Filename
311238
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