SBIR/STTR Research Award

Compact Precision Space IMU

Award identifier 2517f0f6e576320d518a07947fb881f9408bbf637c52036274c2c784da489632Awarding agency National Aeronautics and Space Administration

Award amount

$748,948

Program and phase

SBIR · Phase II

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
INERTIALWAVE INC
Proposal award date
2019-08-12
Contract end date
2021-08-11
UEI
GRH5KCAFEXE3
Solicitation number
SBIR_18_P2
Topic code
S3

Research abstract

Phase I demonstrated key technologies and development work for the Rad Hard frac12; U Compact Precision Inertial Measurement Unit (CIMU).nbsp; Optimized gyro bias compensation including switched drive achieving navigation grade performance using a commercially available TRL9 piezo-transduced Coriolis Vibratory Gyroscope (CVG) sensor integrated with IWrsquo;s digital IWAG control algorithm demonstrated rate noise necessary to attain Attitude Determination with lt;0.1 arc second pointing and arc second level control.nbsp; IW further demonstrated navigation grade north-finding capabilities with a representative IMU block mounted CVG.nbsp; Temperature testing and optimization of thermal bias compensation was also demonstrated.IW successfully replaced the bulky discrete analog CVG controller electronics with IWrsquo;s digital-based low noise ASIC using IWrsquo;s patent pending embedded IWAG control algorithm.nbsp; Full digital closed loop Rate Gyro operation with excellent bias stability was demonstrated.nbsp; Efficacy of IWrsquo;s Radiation Hard by Design (RHBD) method in the ASICrsquo;s CMOS process was demonstrated with successful Mega-Rad level Co60 chamber testing of IWrsquo;s sensor analog front-end (AFE).nbsp; Significant analysis and simulation of Single Event Effects and efficacy of planned SEE hardening for the full RHBD ASIC in planetary orbit and interplanetary radiation environments was completed.nbsp;A full mechanical design and FEA analysis and system design of the IMU was completed with integrated 3-axis ASIC-based CVGrsquo;s, COTS MEMS accelerometers, interface electronics, and mechanical assembly.nbsp; Mechanical modes and thermal characteristics were verified, with more work planned for vibration isolation in Phase II.nbsp;Phase II will design and fabricate a complete RHBD version of the CVG ASIC control.nbsp; We shall then integrate it to resonators and build and test the complete CIMU, achieving significantly smaller size, lighter weight, and much lower power than state-of-the-art space IMUs (e.g. MIMU, SIRU).

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

7 SBIR/STTR records share this UEI (2015–2025). Reported award amounts total $3,172,214. 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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