DocumentCode :
1946821
Title :
Minitact gyroscope-the low cost alternative
Author :
Califano, Herbert T.
Author_Institution :
AlliedSignal Guidance & Control Syst., Teterboro, NJ, USA
fYear :
1994
fDate :
11-15 Apr 1994
Firstpage :
813
Lastpage :
816
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 flexure 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 a miniature two axis gyroscope with a dynamic range of greater than 107. 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; Minitact gyroscope; design to unit production cost; dynamic range; high reliability; integrated product development; low cost device; low noise drift performance; miniature tactical gyro; permanent magnet DC commutated motor; spherical hydrodynamic gas bearing; spinning mass device; torquer; tuned rotor gyroscopes; two axis gyroscope; Commutation; Costs; Gyroscopes; Hydrodynamics; Magnetic levitation; Optical devices; Optical noise; Rotors; Solid state circuits; Spinning;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Position Location and Navigation Symposium, 1994., IEEE
Conference_Location :
Las Vegas, NV
Print_ISBN :
0-7803-1435-2
Type :
conf
DOI :
10.1109/PLANS.1994.303395
Filename :
303395
Link To Document :
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