Unified Interceptor Assignment Algorithms

Award Information
Agency:
Department of Defense
Branch
n/a
Amount:
$999,926.00
Award Year:
2011
Program:
SBIR
Phase:
Phase II
Contract:
HQ0147-11-C-7741
Award Id:
n/a
Agency Tracking Number:
B2-1809
Solicitation Year:
2009
Solicitation Topic Code:
MDA09-026
Solicitation Number:
2009.3
Small Business Information
500 West Cummings Park - Ste 3000, Woburn, MA, -
Hubzone Owned:
N
Minority Owned:
Y
Woman Owned:
N
Duns:
859244204
Principal Investigator:
AdelEl-Fallah
Group Leader, Tracking an
(781) 933-5355
adel@ssci.com
Business Contact:
JayMiselis
Corporate Controller
(781) 933-5355
contracts@ssci.com
Research Institute:
Stub




Abstract
Detecting, localizing, and intercepting one or more missiles during ascent phase presents a daunting theoretical and practical challenge. Scientific Systems Company, Inc. of Woburn, MA, and its subcontractor, Lockheed Martin, propose a foundational, control-theoretic approach to such problems. It is based on the idea of mathematically modeling a multiplatform-multisensor-multitarget system as SINGLE, JOINTLY EVOLVING STOCHASTIC PROCESS. All relevant information regarding behaviors of all sensors, all platforms, and all targets are inherently integrated into the algorithm design at the outset. As a consequence, all major functionsdata fusion, detection, tracking, navigation, and control, etc., are inherently integrated into a single, unified system. Phase I showed the feasibility assessment by simulating rocket trajectories that account for precise targeting and the specific rocket characteristics of medium range rockets, accurate modeling for the I-2 interceptor, and derived multi-firing solution for neutralizing adversary rockets. The results indicated successful intercept and neutralization by detection and tracking using space based IR sensors for the first 50 seconds (with an accuracy of 300 meters) followed by aided tracking utilizing radars on board a destroyer such as AEGIS (with a resulting combined accuracy of 200 meters), and finally the KV IR sensor is utilized for a resulting total accuracy of 20 meters. Phase II work will emphasize development of more mature prototype interceptor-versus-missile algorithms, to be tested using more realistic environments and data, and at more realistic processing speeds. This will include development of a dual-use commercialization plan with special emphasis on developing working relationships with BMD contractors.

* information listed above is at the time of submission.

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