DocumentCode :
3118103
Title :
A monolithic high-g SOI-MEMS accelerometer for measuring projectile launch and flight accelerations
Author :
Davis, Bradford S. ; Denison, Tim ; Kaung, Jinbo
Author_Institution :
US Army Res. Lab., Aberdeen Proving Ground, MD, USA
fYear :
2004
fDate :
24-27 Oct. 2004
Firstpage :
296
Abstract :
Analog Devices (ADI) has designed and fabricated a monolithic high-g acceleration sensor (ADXSTC3-HG) fabricated with the ADI silicon-on-insulator micro-electromechanical system (SOI-MEMS) process. The SOI-MEMS sensor structure has a thickness of 10 μm, allowing for the design of inertial sensors with excellent cross-axis rejection. The high-g accelerometer discussed in this paper was designed to measure in-plane acceleration to 10,000 g while subjected to 100,000 g in the orthogonal axes. These requirements were intended to meet Army munition applications. The monolithic sensor was packaged in an 8-pin leadless chip carrier (LCC-8) and was successfully demonstrated by the U.S. Army Research Laboratory (ARL) as part of an inertial measurement unit during an instrumented-flight experiment of artillery projectiles launched at 15,000 g.
Keywords :
accelerometers; inertial systems; microsensors; military equipment; projectiles; silicon-on-insulator; 10 micron; 10000 g; 100000 g; 15000 g; ADXSTC3-HG; SOI-MEMS; army munitions; artillery projectiles; flight test; high-Q accelerometer; in-plane acceleration sensor; inertial measurement unit; inertial sensor cross-axis rejection; leadless chip carrier; monolithic accelerometer; projectile launch measurement; Acceleration; Accelerometers; Laboratories; Microelectromechanical systems; Packaging; Projectiles; Semiconductor device measurement; Sensor systems; Silicon on insulator technology; Weapons;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Sensors, 2004. Proceedings of IEEE
Print_ISBN :
0-7803-8692-2
Type :
conf
DOI :
10.1109/ICSENS.2004.1426160
Filename :
1426160
Link To Document :
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