SBIR/STTR Research Award

Integrated Micro-Inertial Sensors For GPS Denied Navigation Using Fast-Light Enhanced Ring Laser Gyroscopes and Accelerometers

Award identifier 608f46528c57add7f7def19916d912b2f084e2524ec62f840dfc85a33412208cAwarding agency Department of Defense · Air Force

Award amount

$149,998

Program and phase

SBIR · Phase I

Award year

2013

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
DIGITAL OPTICS TECHNOLOGIES INC
Proposal award date
2013-05-15
Contract end date
2014-02-17
UEI
LBJAKW4NY6A5
Solicitation number
2013.1
Topic code
AF131-065

Research abstract

ABSTRACT: For navigation of space platforms under GPS denied conditions, there is a need for micro-inertial sensors, with better accuracy and smaller volume and weight than the state of the art. We at Digital Optics Technologies (DOT) have been developing a superluminal ring laser gyroscope (SRLG) that can improve the accuracy of rotation sensing by nearly six orders of magnitude. Alternatively, for a given accuracy need, the SRLG can be very small. DOT has also developed the architecture for a superluminal ring laser accelerometer (SRLA), which can achieve a sensitivity of 10 pico-g/root-Hz. Under Phase I, we will demonstrate technical feasibility of realizing a compact inertial measurement unit (IMU) that would comprise three SRLGs and three SRLAs for all-axes sensing, utilizing miniature vapor cells, integrated optical components, detectors and lasers. In addition to miniaturization, a key focus of this effort would be to develop requisite components that would be suitable for space platforms. To this end, we will carry out analysis and test for radiation hardening, extreme temperature variations, and tolerance for high-G situations. Development of a prototype that would meet the size, weight, power and performance goals would be carried out in Phase II. Honeywell, Triad Technology, and International Photonics Consultants would be subcontractors. Dr. Selim Shahriar, inventor of the SRLG and the SRLA and the chief scientific adviser at DOT, will coordinate the overall effort. BENEFIT: Three SRLAs, combined with three SRLGs, can be used to realize a high accuracy IMU that is very compact and light weight. Such an IMU could also be relatively inexpensive. An IMU of this type could have a significant impact on guidance, navigation and control systems for spacecraft, launch vehicles, missiles, kill vehicles, smart munitions, and other applications requiring precision inertial knowledge. Non-DoD applications include spacecraft guidance, navigation and control, as well as commercial aircraft inertial navigation systems

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

44 SBIR/STTR records share this UEI (1999–2026). Reported award amounts total $17,650,801. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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