Integrated Flight Control Systems for Kinetic Kill Vehicles with Novel Internal Actuators

Award Information
Agency:
Department of Defense
Amount:
$749,999.00
Program:
STTR
Contract:
HQ0006-05-C-7261
Solitcitation Year:
2004
Solicitation Number:
N/A
Branch:
Missile Defense Agency
Award Year:
2005
Phase:
Phase II
Agency Tracking Number:
B045-003-0243
Solicitation Topic Code:
MDA04-T003
Small Business Information
OPTIMAL SYNTHESIS INC.
868 San Antonio Road, Palo Alto, CA, 94303
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
Y
Duns:
829385509
Principal Investigator
 P. Menon
 Chief Scientist
 (650) 213-8585
 menon@optisyn.com
Business Contact
 P. Menon
Title: President
Phone: (650) 213-8585
Email: menon@optisyn.com
Research Institution
 UNIV. OF CALIFORNIA-IRVIN
 Kenneth D Mease
 Mech. & Aero. D
Irvine, CA, 92697
 (949) 824-5855
 Nonprofit college or university
Abstract
New internal actuation technologies and integrated design of guidance-control systems for kinetic kill vehicles are proposed. These actuation technologies can be used for KKV trajectory and attitude control in any speed range, both within and outside the atmosphere. Since the actuators are contained entirely within the airframe geometric envelope, and because no mass expulsion is involved, they offer several advantages over conventional aerodynamic control surfaces and reaction control systems. Phase I research demonstrated the feasibility of using three new internal actuation systems for KKV trajectory and attitude control. Target interception within and outside the atmosphere, and engagements containing both endo- and exo-atmospheric trajectory segments were demonstrated. Flight control system robustness was investigated in Monte-Carlo simulations. Optimality of the trajectories was assessed using numerical trajectory optimization methods. Phase II research will develop designs for internally actuated kinetic kill vehicles using more realistic airframe data. Preliminary mechanical designs, actuator sizing, model refinement, integrated guidance-control law designs, trajectory optimization and flight control code generation will be carried out. Low-speed UAV flight demonstration of the actuation concepts will also be conducted. Full-scale development and flight test of an internally actuated kinetic kill vehicle will be undertaken during the Phase III work.

* information listed above is at the time of submission.

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