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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-0216
Agency Tracking Number: N152-094-0231
Amount: $299,991.00
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): 2017-08-28
Award End Date (Contract End Date): 2021-02-25
Small Business Information
3190 Fairview Park Drive Suite 650
Falls Church, VA 22042
United States
DUNS: 010983174
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Subhasis Sarkar Subhasis Sarkar
 Senior Engineer
 (703) 226-4069
 ssarkar@tda-i.com
Business Contact
 Patty Walk
Phone: (703) 226-4064
Email: pwalk@tda-i.com
Research Institution
N/A
Abstract

TDA is proposing to develop a model based technique to automate the verification and validation process of helicopter regime recognition codes in three major steps. In the first step, a list of standardized flight regimes will be developed as this is a pre-requisite for automated verification and validation process, and these may become the recommended standard in the helicopter and HUMS community. In the next step, a helicopter dynamic model will be developed and used to fly various helicopter flight regimes. The parameters of the flight dynamic model will be determined by a nonlinear system identification process utilizing actual HUMS flight data. A virtual pilot will be created that will be used to fly different regimes. In the final step, a verification and validation tool will be developed that will compare the regimes predicted by the regime recognition codes with the actual regimes flown by the simulated helicopter model and will output the misclassification rate, confusion matrix and other relevant statistical measures to quantify the accuracy of the regime recognition algorithms. For the purposes of this program, TDA will use the SH-60B helicopter to generate example results and will extend to other helicopter platforms later.

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

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