DocumentCode
2741232
Title
SiMMATM accelerometer for inertial guidance and navigation
Author
Leonardson, Ron ; Foote, Steve
fYear
1998
fDate
20-23 Apr 1998
Firstpage
152
Lastpage
160
Abstract
This paper presents recent accomplishments in SiMMATM silicon micromachined accelerometers using vibrating beam accelerometer (VBA) technology, focusing on achieving navigation grade performance with reduced size and lower cost. Guidance and navigation system applications have continued to require smaller, lower-cost accelerometers. High reliability and long term stability in temperature modeled systems are also in demand. Available navigation grade accelerometers cannot meet all of these inertial measurement unit (IMU) requirements. Direct digital system usage of the SiMMATM accelerometer output reduces system level IMU cost by eliminating the need for digitizers (or A/D conversion), their analog calibration costs, resolution limitations, and their instability. High performance silicon micromachined vibrating beam SiMMATM accelerometers best meet these next-generation IMU accelerometer requirements. The SiMMATM accelerometer presented is a silicon micromachined VBA that converts an applied analog acceleration force directly into frequency modulated electronic signals for direct use in digital strapdown systems. Basic theory of operation is presented. New accelerometer development uses a monolithic single proof mass with integrated dual double-ended tuning forks (DETFs), for differential detection and improved common mode performance. Presently, accelerometer and integrated electronics are packaged in a hermetic metal case for long term reliability with gas damping for vibration control. Units have been designed and tested for programs comprising tactical (100 g) through navigation (20 g) range and performance grade applications
Keywords
accelerometers; inertial navigation; microsensors; packaging; reliability; silicon; stability; FEA; Si; Si micromachined accelerometers; SiMMA accelerometer; differential detection; digital strapdown systems; finite element analysis; frequency modulated electronic signals; gas damping; hermetic metal case; high reliability; inertial guidance; integrated dual double-ended tuning forks; long term stability; mechanism geometry optimization; monolithic single proof mass; navigation; temperature effects; thermal modeling; vibrating beam accelerometer technology; vibration control; Acceleration; Accelerometers; Calibration; Costs; Digital systems; Measurement units; Navigation; Silicon; Stability; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, IEEE 1998
Conference_Location
Palm Springs, CA
Print_ISBN
0-7803-4330-1
Type
conf
DOI
10.1109/PLANS.1998.670036
Filename
670036
Link To Document