Design and Optimization of Radar Systems to Assist Rotorcraft Piloting in Adverse Environments

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-09-C-0382
Agency Tracking Number: N082-141-0010
Amount: $749,999.00
Phase: Phase II
Program: SBIR
Awards Year: 2009
Solicitation Year: 2008
Solicitation Topic Code: N08-141
Solicitation Number: 2008.2
Small Business Information
3015 Village Office Place, Champaign, IL, 61822
DUNS: 782768977
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Robert Kipp
 Chief Scientist
 (312) 431-7413
Business Contact
 Matthew Miller
Title: President
Phone: (217) 363-3396
Research Institution
Rotorcraft are increasingly turning toward high-resolution Ka- through W-band radar sensors that can image terrain and obstructions but also see through the particulates that confound infrared and optical sensors, such as sand, ocean spray, and fog. As with any onboard sensor, designers must consider the antenna/platform interaction, and mature tools exist to address this type of problem. However, at these wavelengths, airborne vehicles can span several thousand wavelengths. This is well beyond the capability of any full-wave electromagnetic solver. While asymptotic techniques are practical here, they are powerless to model the antennas, themselves. We propose to develop two novel techniques for integrating asymptotic and full-wave methods that can solve the end-to-end antenna/platform integration problem. One technique folds physical optics directly into method-of-moments to greatly expand the size of problem it can handle, but without compromising accuracy. The other splits the problem into small (full-wave) and large (asymptotic) regions, the novelty being the ease of integration that allows both solution regimes to fully couple. The Phase I effort focused on proof-of-concept and comparative evaluation of these two techniques. In Phase II, we will fully develop both techniques, including commercial-grade GUIs.

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

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