NASA STTR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- T4.01-3162
SUBTOPIC TITLE:
 Information Technologies for Intelligent and Adaptive Space Robotics
PROPOSAL TITLE:
 Scalable and Distributed Inertial Navigation Systems
SMALL BUSINESS CONCERN (SBC):
RESEARCH INSTITUTION (RI):
Name:   CU Aerospace, LLC
Name:   University of Illinois at Urbana-Champaign
Street:  301 North Neil Street, Suite 502
Street:  312 Talbot Laboratory MC 236, 104 S. Wright St.
City:   Champaign
City:   Urbana
State/Zip:  IL  61820-3169
State/Zip:   IL 61801 - 2958
Phone:  (217) 239-1702
Phone:   (217) 244-3126


Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
David Carroll
carroll@cuaerospace.com
301 North Neil Street, Suite 502 Champaign, IL 61820 - 3169
(217) 239-1703

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
David Carroll
carroll@cuaerospace.com
301 North Neil Street, Suite 502 Champaign, IL 61820 - 3169
(217) 239-1703
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 4
Technical Abstract

Current state of the art inertial measurement units (IMUs) co-locate a set of accelerometers and gyroscopes into a single package. CU Aerospace (CUA), in partnership with the University of Illinois, propose to develop a scalable and distributed IMU for space robotics and CubeSat applications. The user can choose to include an arbitrary number of inertial sensors beyond the minimal number of sensors required for inertial navigation (3 gyroscopes and 3 accelerometers). This scalability enables both improved measurement resolution and system redundancy. The distributed nature of the system means that sensors can be placed arbitrarily by the user as needed in their design, under the constraint that each axis is measured by at least one accelerometer and gyroscope. This technology enables space-constrained systems to leverage redundant inertial sensors for fault detection and isolation (FDI). Beyond the systems engineering benefits of this system, distributing the sensors is grounded by previous research that suggests it will reduce the total noise of its output measurements. This technology can potentially be used in most robotic systems currently using an inertial navigation system. However, the best applications of this technology are in space constrained robots that can benefit from accurate state estimates or fault tolerant systems.

Potential NASA Applications

Distributed and scalable inertial measurement units can enable missions where MEMS components are failure prone. The technology provides emerging areas of CubeSat robotics and assembled structures with flexible in system layout. This technology can be used to reduce sensor noise while efficiently using space for human assisted robots aboard the international space station and or on autonomous or human assisted terrestrial rovers.

Potential Non-NASA Applications

The best applications of this technology, however, is in space constrained robots that can benefit from accurate state estimates or fault tolerant systems. For example, in the natural gas industry, improved state estimates will translate into a better ability to pinpoint the location of problems prior to the excavation of a pipeline. Our concept can also improve pedestrian location technology by leveraging IMUs on multiple wearable devices for dead reckoning.


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