Small Business Innovation Research/Small Business Tech Transfer
Physical Modeling for Anomaly Diagnostics and Prognostics, Phase II
Project Introduction
Ridgetop developed an innovative, model-driven anomaly diagnostic and fault characterization system for electromechanical actuator (EMA) systems to mitigate catastrophic failures. Ridgetop developed a MIL-STD-1553 bus monitor and a MIL-STD-1553 bus controller that simulates the aircraft data bus, reads the environmental (i.e., altitude) and operational (i.e., response of system) data of a system and determines if a fault is manifesting; and if true determines the root cause and symptoms of the fault. Once an anomaly is detected, the Model-based Avionic Prognostic Reasoner (MAPR) solves a user-outlined state-space model, symbolically, using a Gauss-Newton optimization method and the information from the MIL-STD-1553 bus. This algorithm outputs a list of best fitting parameters to match the command to the actual performance. Rules are programmed in, based on results from principal component analysis . The rules determine both fault mode and the severity of that fault. The rules can distinguish between two failure modes: Mechanical jam and MOSFET failure, and healthy. The real-time processing will allow for critical evolutions in flight safety and provides a game-changing approach to condition-based maintenance. Once deployed, flight safety can be improved by allowing the on-board flight computers to read from the MAPR and update their control envelope based on its evaluations, reducing damage propagation and increasing operational safety. In Phase 2, we will develop a functioning ground-based prototype of the technology to show the efficacy of the method. A ground-based version of the tool is the best candidate for development to ease adoption by testing in a low-risk environment; this tool will be demonstrated at the end of Phase 2. The MAPR concept is also applicable to any system with a state-space representation but at this point it has been developed with EMAs in mind. The MAPR prototype is at TRL 5 and will reach a TRL 7 by the end of Phase 2.
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Anticipated Benefits
Target markets for non-NASA commercial applications that utilize standard MIL-STD-1553, ARINC 429 communications between subsystems, and include government and commercial aerospace, automotive markets, satellites, and factory automation applications. For the aerospace market, Ridgetop will strategically partner with Boeing to integrate the technology at the component level (physical product) and the system level (aircraft platform). Leveraging existing relationships with key auto manufacturers such as Daimler, Ridgetop plans to integrate the proposed technology to add value to existing on-board diagnostic platforms with the consolidated sensor network and advanced reporting/data capabilities. The UAV market is growing, evidenced by increased demands and requirements for operational efficiency and duration. Recent breakthroughs in UAV power systems have presented a dynamic integration opportunity for the proposed fault detection software. From a marketing analysis, the total forecasted revenues from these markets are projected to reach $39 million over five years. Vehicles within the Europa mission, the International Space Station (ISS), and Mars Exploration Rover Project. The Europa mission has been designated by the Decadal Study as the highest-priority flagship mission for the next decade, and the Europa Geophysical Explorer (EGE) is likely to be the next large mission to the outer planets after Cassini. Applications in this program include fault-tolerant EMAs. Ridgetop plans to collaborate in the NASA IVHM program to aid in the detection, diagnosis and prognosis of avionics faults and malfunctions, actuator failure and damage, and avionics transient effects resulting from operation in a harsh environment (neutron particles, electromagnetic fields, lightning), including the Deep Space mission, and Exploration Technology Development Program Integrated Systems Health Management (ETDP-ISHM) and the X-37 program.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Ridgetop Group, Inc. | Lead Organization |
Industry
Women-Owned Small Business (WOSB)
|
Tucson, Arizona |
Ames Research Center
(ARC)
|
Supporting Organization | NASA Center | Moffett Field, California |
Primary U.S. Work Locations
-
Arizona
-
California
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Organization:
- Ridgetop Group, Inc.
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Project Duration
Start: Jun 2011
End: May 2013
Technology Maturity (TRL)
| Start: | 5 |
| Current: | 7 |
| Estimated End: | 7 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX11 Software, Modeling, Simulation, and Information Processing
- TX11.5 Mission Architecture, Systems Analysis and Concept Development
- TX11.5.2 Tools and Methodologies for Performing Systems Analysis
Target Destination
Earth
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