NASA SBIR 2020-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 20-1- S5.05-6754
SUBTOPIC TITLE:
 Fault Management Technologies
PROPOSAL TITLE:
 Autonomous Coordinated Operations Response Network for Fault Detection, Isolation, and Response
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Blue Sun Enterprise, Inc.
1942 Broadway Street, Suite 314
Boulder, CO 80302
(720) 394-8897

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Dr. Christopher Grasso
E-mail:
cgrasso@bluesunenterprises.com
Address:
1942 Broadway Street Suite 314 Boulder, CO 80302
Phone:
(720) 236-5656

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)

Name:
Christopher Grasso
E-mail:
contact@bluesunenterprises.com
Address:
1942 Broadway Street, Suite 314 Boulder, CO 80302 - 5233
Phone:
(720) 394-8897
Estimated Technology Readiness Level (TRL) :
Begin: 1
End: 4
Technical Abstract (Limit 2000 characters, approximately 200 words)

The Autonomous Coordinated Operations Response Network (ACORN) is a state-based approach to FDIR built atop advanced sequencing capabilities currently available in the marketplace. ACORN offers a standardized method for designing, implementing, and running fault protection across disparate spacecraft. The approach uses graphical representations of state machines which manage various subsystems of the spacecraft. The runtime version of state machines coordinate together using guard conditions on transitions. These state machines identify and respond to faults at the component, intermediate, and system levels. Identification of fault conditions is based on telemetry values and sequence global variable values written to by flight software during runtime.

The state-based design of ACORN enforces flight rules and other requirements, operating the spacecraft in a constraint-oriented manner. Responses take the form of spacecraft commands and sequence block invocations, which are implementations found on all spacecraft. Since ACORN runs onboard the spacecraft, it has immediate access to all of the telemetry necessary to detect faults.

ACORN specifications are mission-independent. If a mission lacks a sufficiently powerful sequencing capability to implement the specification, the ACORN process is still extremely useful as a high-level design specification for custom components to be implemented, and allows a standardized capability to be used. Should the target mission feature a sequencing capability with an ACORN translation tool, the specification is automatically translated into an executable set of sequencing components that fully implement the desired detections and capabilities.

Advantages:
1. cross-mission
2. cross-platform
3. inheritable
4. efficient specification
4. fast response times (on board)
6. emergent behavior
7. low cost
8. transparent
9. layered interfaces
10. iterative process

 

Potential NASA Applications (Limit 1500 characters, approximately 150 words)

ACORN is applicable to any space mission performing on-board fault protection. The potential for standardized, inexpensive, extensible, transparent fault protection system using a graphical notation can be targeted at the whole range of LEO, GEO, and interplanetary missions, large and small.

Human spaceflight could utilize ACORN for on-board spacecraft FDIR, allowing the system to autonomously determine faults and issue corrections without the time-consuming intervention of the crew.

 

Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words)

ACORN works with any flight software core. It could be applied to non-NASA spacecraft: DoD, NOAA, and ESA missions are prime candidates. Small commercial missions could reduce costs by reducing expensive fault protection personnel time.

 

Duration: 6

Form Generated on 06/29/2020 21:07:43