A Monolithic High-G SOI-MEMS Accelerometer for Measuring Projectile Launch and Flight Accelerations
Author(s) -
Bradford S. Davis,
Timothy Denison,
Jinbo Kuang
Publication year - 2005
Publication title -
shock and vibration
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.418
H-Index - 45
eISSN - 1875-9203
pISSN - 1070-9622
DOI - 10.1155/2006/793564
Subject(s) - accelerometer , microelectromechanical systems , artillery , silicon on insulator , projectile , acceleration , inertial measurement unit , engineering , electrical engineering , materials science , aerospace engineering , optoelectronics , silicon , physics , computer science , classical mechanics , artificial intelligence , metallurgy , quantum mechanics
Analog Devices (ADI) has designed and fabricated a monolithic high-g acceleration sensor (ADXSTC3-HG) fabricated with the ADI silicon-on-insulator micro-electro-mechanical system (SOI-MEMS) process. The SOI-MEMS sensor structure has a thickness of 10 um, 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 US Army Research Laboratory (ARL) as part of an inertial measurement unit during an instrumented flight experiment of artillery projectiles launched at 15,000 g
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