Compact Inertial Measurement System

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$99,918.00
Award Year:
2007
Program:
SBIR
Phase:
Phase I
Contract:
HQ0006-07-C-7706
Agency Tracking Number:
B063-022-1054
Solicitation Year:
2006
Solicitation Topic Code:
MDA06-022
Solicitation Number:
2006.3
Small Business Information
APPLIED TECHNOLOGY ASSOC.
1300 Britt SE, Albuquerque, NM, 87123
Hubzone Owned:
N
Socially and Economically Disadvantaged:
Y
Woman Owned:
N
Duns:
081475873
Principal Investigator:
HENRY SEBESTA
Principal Investigator
(505) 767-1202
henry.r.sebesta@aptec.com
Business Contact:
Jeffrey Stein
Director-Contracts, Finance & Admin
(505) 767-1231
stein@aptec.com
Research Institution:
n/a
Abstract
Applied Technology Associates (ATA) proposes to develop a compact inertial measurement system (CIMS) by combining two inertial rate sensing devices. One rate sensor uses magnetohydrodynamics (MHD) for high frequency motion measurement and is denoted the Angular Rate Sensor (ARS). The second sensor is a new micro-electro-mechancial system (MEMS) gyro denoted the Disk Resonant Gyro (DRG) and is used for low frequency motion measurement. In addition to combined ARS/DRG motion sensing, the CIMS also exploits FPGA-based electronics for multi-sensor signal conditioning and fusion. A complete, autonomous attitude determination system is achieved by optionally including a stellar camera unit / star tracker to provide calibration and inertial sensor drift compensation. Depending on performance requirements, other aiding sensors (magnetometers, horizon sensors, etc) may be substituted for the stellar camera. CIMS achieves motion measurement sensitivity at 5 arcsecs (25 microrads) or less over the bandwidth DC-100 Hz. Measurement noise of CIMS above 1 Hz is estimated to be less than 1 microrad. The mass of CIMS is less than 1.5 kg and power required under 2 W.

* information listed above is at the time of submission.

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