MEMS Annular Rotating Sensor (MARS)

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$749,998.00
Award Year:
2003
Program:
SBIR
Phase:
Phase II
Contract:
N0017803C1059
Agency Tracking Number:
02-0507
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
ARCHANGEL SYSTEMS, INC.
1500 Pumphrey Ave., Auburn, AL, 36832
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
844905208
Principal Investigator:
Victor Trent
Senior Research Engineer
(334) 826-8008
victor@archangel.com
Business Contact:
Kitty Greene
President
(334) 826-8008
kitty@archangel.com
Research Institution:
n/a
Abstract
A MEMS Rotating Annular Sensor (MARS) is proposed which senses rotation velocities and accelerations in one discrete time sensor. Differential capacitance measured at various points about the annulus permit a single MARS to measure accelerations in threedegrees of freedom and rotational velocities in two, missing only the angular velocity about the local z axis. Two MARS systems can be used for full three axis inertial measurements and provide redundancy in all three accelerations and one rotationalvelocity measure. With built-in processing capability, the MARS system results in an extremely small, low-cost yet robust inertial measurement system. Output of the MARS system will be available in various digital serial formats.The MARS system has been designed to have four modes of operation: Storage, Start-up, Nominal Operation and Shut-down. To enable reliable use, each mode is operated in a controlled operation enabling the device to handle very large g loads withoutfailure. Sensing rotational rates up to 1000 degrees per second and accelerations up to 15,000 g are anticipated with the device. Due to the differential nature of the device, noise and temperature effects are expected to be minimal when compared toconventional MEMS devices.

* information listed above is at the time of submission.

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