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Simulation Tool to Intercept Multiple Missiles Employing Quick and Random…

Award Information

Agency:
Department of Defense
Branch:
Missile Defense Agency
Award ID:
81788
Program Year/Program:
2007 / SBIR
Agency Tracking Number:
B063-049-1043
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Princeton Satellite Systems
6 Market St. Suite 926 Plainsboro, NJ 08536
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 2007
Title: Simulation Tool to Intercept Multiple Missiles Employing Quick and Random Evasive Flight Path
Agency / Branch: DOD / MDA
Contract: W9113M-07-C-0031
Award Amount: $99,796.00
 

Abstract:

This proposal is for the development of a versatile, computationally-efficient simulation tool for integrating flight path data from missile interceptors and analyzing defensive missile scenarios. The simulation tool will provide a user-friendly platform for design and testing of cooperative missile-interception techniques. We also propose to develop innovative cooperative control algorithms for multiple interceptors pursuing multiple missiles. Our cooperative control algorithms will be based on using artificial potentials for determining command accelerations for individual interceptors. The artificial potentials framework provides a systematic procedure for designing and implementing formation control and reconfiguration. We will combine artificial potential based cooperative control with modern target detection and missile guidance techniques to create an integrated solution for cooperative missile interception. This will be a step towards developing reliable technology for countering missiles that are specifically designed to elude interceptors via quick and random flight path changes. The simulation tool will be modular in nature, and will incorporate all aspects of cooperative missile interception including search-surveillance-engage modes, formation control and reconfiguration, inter-interceptor communication limitations, resource management and flight path data fusion. Interceptor performance constraints such as minimum turning radius and maximum velocity, as well as time-varying communication topologies will be accounted.

Principal Investigator:

Pradeep Bhatta
Senior Technical Staff
6092799606
pradeep@psatellite.com

Business Contact:

Michael Paluszek
President
6092799606
map@psatellite.com
Small Business Information at Submission:

PRINCETON SATELLITE SYSTEMS
33 Witherspoon Street Princeton, NJ 08542

EIN/Tax ID: 223192263
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No