SBIR/STTR Research Award

Compact and Integrated IMU for GPS Denied Navigation Using Fast-Light Gyroscopes and Accelerometers

Award identifier 1cfb932c33ef4e907bbe6408fba514bc49d2f389b23cf5615d435d2000a0957cAwarding agency Department of Defense · Air Force

Award amount

$999,893

Program and phase

SBIR · Phase II

Award year

2014

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
DIGITAL OPTICS TECHNOLOGIES INC
Proposal award date
2014-07-17
Contract end date
2015-10-11
UEI
LBJAKW4NY6A5
Solicitation number
2011.2
Topic code
AF112-100

Research abstract

ABSTRACT:For GPS denied navigation, there is a need for developing inertial measurement units (IMU), employing gyroscopes and accelerometers, with better accuracy and/or smaller volume and weight than the state of the art.Under Phase I, we have established the feasibility of realizing a superluminal ring laser gyroscope (SRLG) and a superluminal ring laser accelerometer (SRLA), based on diode-pumped alkali lasers (DPALs), augmented by a fast-light Raman cells.The SRLG can improve the accuracy of rotation sensing by nearly five orders of magnitude.Alternatively, for a given accuracy need, the SRLG can be very small.The SRLA can be very compact, and achieve a sensitivity of 10 pico-g/Hz.The primary goal of the Phase II effort is to demonstrate a prototype IMU that would house three SRLGs and three SRLAs for 3-axis rotation and acceleration sensing, utilizing miniature vapor cells and frequency-stabilized lasers.The prototype will be tested and analyzed in order to identify any possible technical hurdles in meeting the size, weight, power and performance goals stated in the solicitation, as well as to address applicability to weapon systems and aircraft/spacecraft environments.Northwestern University will participate as a subcontractor.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 andlight 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, commercial aviation, emergency response in urban canyons, mining and tunneling operations, and maritime operations.

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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