DocumentCode
3111629
Title
A miniature, gun-hard MEMS IMU for guided projectiles, rockets and missiles
Author
Scaysbrook, I.W. ; Cooper, S.J. ; Whitley, E.T.
Author_Institution
BAE SYSTEMS, Plymouth, UK
fYear
2004
fDate
26-29 April 2004
Firstpage
26
Lastpage
34
Abstract
BAE SYSTEMS is a leading provider of inertial sensors and systems, including silicon-MEMS inertial based products to automotive, commercial and military markets. BAE SYSTEMS is developing a miniature MEMS inertial measurement unit. SiIMU02™ is capable of surviving and performing after the massive shock and vibration environment of a guided projectile gun-launch event, and is small enough to fit into next generation small caliber guided rockets and missiles. This paper explains the logical progression from the first generation SiIMU01™, which is now in production, to the second generation SiIMU02™, as the next step along a development roadmap to even smaller and better performing MEMS IMUs in the near future. The IMU architecture is presented, as are results of initial prototype performance testing and gun firing trials. The emerging guided projectile and rocket programs are posing new challenges for inertial measurement units. These special requirements, and how they are solved by the unique combination of sensor technology and IMU architecture employed in SiIMU02™, are explained.
Keywords
inertial navigation; micromechanical devices; missile guidance; missiles; rockets; guided projectile gun-launch event; guided projectiles; inertial sensors; miniature gun-hard MEMS IMU; missiles; rockets; silicon-MEMS inertial based products; Automotive engineering; Electric shock; Measurement units; Micromechanical devices; Missiles; Production; Projectiles; Prototypes; Rockets; Sensor systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 2004. PLANS 2004
Print_ISBN
0-7803-8416-4
Type
conf
DOI
10.1109/PLANS.2004.1308970
Filename
1308970
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