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High Performance Resonator Fiber Optic Gyro Made of Air Core Fiber

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0006-08-C-7809
Agency Tracking Number: B073-052-0730
Amount: $99,987.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: MDA07-052
Solicitation Number: 2007.3
Timeline
Solicitation Year: 2007
Award Year: 2008
Award Start Date (Proposal Award Date): 2008-02-13
Award End Date (Contract End Date): 2009-08-13
Small Business Information
15 Cabot Road
Woburn, MA 01801
United States
DUNS: 004841644
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jing Zhao
 CTO
 (781) 935-1200
 jzhao@agiltron.com
Business Contact
 Lisa Boardman
Title: Contract Administrative Assistant
Phone: (781) 935-1200
Email: lboardman@agiltron.com
Research Institution
N/A
Abstract

Agiltron proposes an innovative resonant fiber optic gyro (RFOG) based on air-core optical fiber achieving high performance, compact size, lightweight and low fabrication cost. The proposed gyro uniquely combines the advantages of high finesse of a ring laser gyro (RLG) and the advantages of long optical path and miniature package of interferometer fiber optic gyro (IFOG). Critically, the utilization of air-core fiber dramatically reduces the undesirable nonlinear effects inducing long term drift and short term noise in silica fiber caused by the Kerr effect, Faraday effect, and Rayleigh backscattering by a factor of up to 500, and the Shupe thermal effect by factor 3 to 10 due to the light propagating inside of air core rather than silica. Moreover, the RFOG can provide high sensitivity with short fiber length and use a closed loop configuration and narrow bandwidth laser to detect the frequency shift, resulting in smaller drift and high signal to noise ratio. Phase I will identify the critical technology challenges, synthesize advanced architectures, perform concept feasibility analysis, build the basic resonator module, and define the Phase II approach.

* Information listed above is at the time of submission. *

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