DocumentCode
2462672
Title
An integrated MEMS inertial measurement unit
Author
Cardarelli, Donato
Author_Institution
Milli Sensor Syst. & Actuators, Inc., W. Newton, MA, USA
fYear
2002
fDate
2002
Firstpage
314
Lastpage
319
Abstract
With MEMS technologies, instrument subcomponents are integrated in the design to form individual gyroscopes and accelerometers on a single chip. This replaces the assembly of individual subcomponents which forms conventional instruments. Similarly, MEMS instrument components can be integrated to form complete inertial measurement units (IMUs). Integration is the only practical approach to realizing low cost and small size units, largely because both instrument and IMU assembly and instrument alignment tasks are eliminated. The obstacle to success is the lack of fabrication process maturity which limits the yield of satisfactory devices which, in turn, very severely limits the yield and escalates the cost of systems that require six working devices on the same chip. The solution to this problem is to base the IMU on instruments with a common design so that the fabrication process variations produce similar effects on each of the instruments. The IMU performance can be optimized by exploiting the commonality between instruments.
Keywords
accelerometers; electric sensing devices; gyroscopes; inertial navigation; micromachining; microsensors; military equipment; military systems; IMU assembly; IMU performance; MEMS instrument component integration; MEMS technology; accelerometers; fabrication process maturity; fabrication process variations; gyroscopes; inertial measurement units; instrument alignment tasks; instrument assembly; instrument commonality; instrument design; instrument subcomponents; integrated MEMS inertial measurement unit; process yield; single chip design; systems cost; Accelerometers; Assembly; Costs; Epitaxial layers; Fabrication; Gyroscopes; Instruments; Measurement units; Micromechanical devices; Silicon;
fLanguage
English
Publisher
ieee
Conference_Titel
Position Location and Navigation Symposium, 2002 IEEE
Print_ISBN
0-7803-7251-4
Type
conf
DOI
10.1109/PLANS.2002.998924
Filename
998924
Link To Document