Small Business Innovation Research/Small Business Tech Transfer
Extensible Data Set Architecture for Systems Analysis, Phase I
Project Introduction
The process of aircraft design requires the integration of data from individual analysis of aerodynamic, structural, thermal, and behavioral properties of a flight vehicle. At present, there is no simple way to integrate the results of the analyses early in the design process. Aurora Flight Sciences and the Massachusetts Institute of Technology Aerospace Computational Design Laboratory propose to create a system level analysis framework called the Extensible Data Set Architecture to facilitate this integration, and therefore provide rapid system-wide impact assessment of design changes to a flight vehicle. The Extensible Data Set Architecture (EDSA) is a generic data storage structure ready for use by a diverse and extendable set of software tools and codes. The EDSA can be arbitrarily extended to allow additional functionality and provides a natural framework for future development of aerospace systems. The framework includes as part of its structure the relevant metadata for ensuring version control, traceability, context-specific documentation, and interface data for relevant tools, while providing a simple structure for extending an existing data set to transparently include new members. The four primary components of this framework will be 1) an extensible data set used by all codes and analysis tools to store and exchange relevant information; 2) a tool set which can take advantage of the data set, made up of both existing programs and user defined vehicle specific codes; 3) a controller which provides organization, operates the tools, and manages iteration and optimization of the design, and 4) a display code which presents the results of the analysis to the user.
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Anticipated Benefits
Modern aircraft system engineering strives to integrate subsystems into an efficient concept which responds to the needs of the vehicle's mission. As these designs become more tightly coupled, such that changes to a subsystem rapidly propagate through the vehicle, the design process must adapt to show the interactions between subsystems as early as possible in the design process, and to facilitate communication between traditionally separate engineering disciplines. The primary financial incentive for Aurora's development of this system is the increased productivity associated with use of the tool. Aurora completes on average 4 preliminary aircraft designs per year, each taking up to ¬Ω a man-year. This tool is anticipated to speed preliminary analysis by as much as 50% as the system matures, with potential net benefit to Aurora of up to 50,000 per design. This tool is also expected to generate more business for Aurora by improving our turnaround for tightly coupled system engineering and increasing Aurora's ability to respond to needs in the military and civilian UAV markets. The implementation of this architecture will speed turnaround time for NASA Dryden flight test safety simulation, and allow for rapid evaluation of design concepts and collaborative effort between disciplines and across geographical distances. The proposed framework will facilitate multi-disciplinary analysis by giving each discipline's preferred tool a common model source, and allow the results of one calculation to be rapidly integrated into another. The framework will allow systems engineers to ensure consistency between disciplinary analyses through the use of universal version control as applied to design changes. The framework will facilitate communication between geographically disparate users by allowing updated model data to be seamlessly pushed to various users, preventing outdated model data from being used for any new work. Additionally, the framework will give the engineer unprecedented access to complete system information during preliminary design, with a choice of display tools which is independent of the origin of the data.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Armstrong Flight Research Center
(AFRC)
|
Supporting Organization | NASA Center | Edwards, California |
| Massachusetts Institute of Technology (MIT) | Supporting Organization | Academia | Cambridge, Massachusetts |
Primary U.S. Work Locations
-
California
-
Massachusetts
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Responsible Program:
- Small Business Innovation Research/Small Business Tech Transfer
Project Management
Program Director:
Program Manager:
Principal Investigator:
- James Houghton
Project Duration
Start: Jan 2010
End: Jan 2011
Technology Maturity (TRL)
| Start: | 2 |
| Current: | 4 |
| Estimated End: | 4 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TX11 Software, Modeling, Simulation, and Information Processing
- TX11.4 Information Processing
- TX11.4.1 Science, Engineering, and Mission Data Lifecycle
Target Destination
Earth
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