SBIR/STTR Research Award

Chip-Scale Active Fast Light Gyroscope and Accelerometer using Integrated Photonic Technology

Award identifier ae8dce37f768298adc44ddba1093ecca30475ae974767188c32c5297035df8e3Awarding agency National Aeronautics and Space Administration

Award amount

$124,861

Program and phase

SBIR · Phase I

Award year

2018

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
DIGITAL OPTICS TECHNOLOGIES INC
Proposal award date
2018-07-27
Contract end date
2019-02-15
UEI
LBJAKW4NY6A5
Solicitation number
SBIR_18_P1
Topic code
S3

Research abstract

The fast-light effect in a cavity, in the active or passive mode, has emerged as an important mechanism for enhancing the sensitivity of many devices. Recently, we have been investigating the development of gyroscopes and accelerometers using the active mode, in which the cavity is a Fast-Light Ring Laser (FLRL). Specifically, we have demonstrated, on a table-top, a pair of counter-propagating FLRL’s, with one of the cavity mirrors mounted on a metallic diaphragm, thus realizing an Active Fast Light Gyroscope and Accelerometer (AFLOGA). In this system, the anomalously dispersive gain is produced by a pair of Rb vapor cells, each containing two isotopes of Rb. We have seen an enhancement in sensitivity by a factor of nearly three orders of magnitude. In order to increase the sensitivity further, and demonstrate the corresponding improvements in the minimum measurable rates of rotation or acceleration, it is necessary to achieve quantum noise limited operation, by enhancing the robustness of the system. To this end, we here propose to develop a miniature AFLOGA, using chip-scale components at Rb wavelengths of 780/795 nm. The components include lasers, modulators, detectors, waveguides, and optical isolators, integrated on a single chip. GaAsP Quantum Wells (QWs) will enable the realization of the active photonic components. In sections for the passive components, the QWs would be disordered to minimize optical losses. A resonator containing two miniature vapor cells will be used as the cavity for the two FLRLs. The chip-mounted components will be interconnected with the cavity, as well as additional electronics on a printed circuit board. In Phase I, we will develop a detailed design of the chip-scale AFLOGA and demonstrate functionality of key components. In Phase II, we will demonstrate operation of an AFLOGA with a million-fold improvement in precision, and then use copies thereof to demonstrate a three-axes Fast-Light Inertial Measurement Unit (FLIMU).

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.

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

National Aeronautics and Space Administration

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