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Model-Based Tool for the Automatic Validation of Rotorcraft Regime Recognition Algorithms

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-17-C-0217
Agency Tracking Number: N152-094-0432
Amount: $249,999.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: N152-094
Solicitation Number: 15.2
Timeline
Solicitation Year: 2015
Award Year: 2017
Award Start Date (Proposal Award Date): 2017-08-24
Award End Date (Contract End Date): 2021-04-05
Small Business Information
2350 Commonwealth Dr. Suite B
Charlottesville, VA 22901
United States
DUNS: 796533102
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Jason Hull Jason Hull
 Member, Spire Innovations LLC
 (434) 962-2639
 jason.hull@spire-innovations.com
Business Contact
 Jeffrey Monaco
Phone: (434) 284-0587
Email: jeffrey.monaco@spire-innovations.com
Research Institution
N/A
Abstract

Accurate and reliable Regime Recognition (RR) algorithms are a key enabling technology for a Condition Based Maintenance (CBM) program, which tailors the service profile to individual vehicles based on actual aircraft usage. In general, production RR algorithms with the required accuracy to provide such usage information do not exists yet, in part because of the expense and human involvement currently required to develop and independently verify and validate the candidate approaches. A dominant cost factor is the need to perform numerous flight tests and the associated time-consuming V&V process of manually comparing RR algorithm results with flight test data. The proposed Independent Verification & Validation (IV&V) software tool addresses both of these cost drivers by (i) automating the analysis and its attendant quantitative statistics for an objective measure of performance, both absolute and relative to alternative RR codes under consideration and (ii) automating the process of obtaining an information rich set of data that feeds the IV&V logic through novel combinations flight-test data , and of high-fidelity, model-based rotorcraft simulation maneuvers instantiated by the tool.

* Information listed above is at the time of submission. *

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