Integrated Guidance and Control of Moving-Mass Actuated Kinetic Warheads

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: N0017803C3061
Agency Tracking Number: 01-0417
Amount: $999,910.00
Phase: Phase II
Program: SBIR
Awards Year: 2003
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
4966 El Camino Real, Suite 108, Los Altos, CA, 94022
DUNS: 829385509
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 P. Menon
 Research Scientist
 (650) 210-8282
Business Contact
 P. Menon
Title: President
Phone: (650) 210-8282
Research Institution
Methods for integrated design of guidance and control systems of kinetic warheads utilizing moving-mass actuators are proposed. Moving mass actuation can be used in any speed range, both in the atmosphere as well as outside it, as long as there is a force,either aerodynamic or propulsive, acting on the vehicle. Since they are contained entirely within the airframe geometric envelope, and because no mass expulsion is involved, moving-mass actuation offers several advantages over conventional aerodynamiccontrol surfaces and reaction control systems. Phase I SBIR work developed a high fidelity simulation model of a kinetic warhead with three moving-mass actuators. Both conventional and integrated flight control systems were then designed using this model.Interception of non-maneuvering and weaving targets in both atmospheric and exo-atmospheric conditions were demonstrated. Phase II research will develop the moving-mass actuation concept to the point where prototype development for a specific mission canbe contemplated. Preliminary mechanical designs, actuator sizing, model refinement, integrated guidance-control law designs and flight control code generation for a prototype vehicle will be carried out during the Phase II work. Full-scale development andflight test of a moving-mass actuated kinetic warhead will be undertaken during the Phase III work.

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

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