| ||The technology within this topic is restricted under the International Traffic in Arms Regulation (ITAR), which controls the export and import of defense-related material and services. Offerors must disclose any proposed use of foreign nationals, their country of origin, and what tasks each would accomplish in the statement of work in accordance with section 3.5.b.(7) of the solicitation.|| Objective: ||Develop a system integration environment for design, analysis, and optimization of airborne directed energy systems.
|| Description: ||The design of airborne directed energy systems presents a challenge due to the use of high-power, tightly-regulated, low-efficiency loads and the size, weight, and thermal constraints of the aircraft. Although steady-state analysis and component optimization is vital in the initial design phase, these techniques may yield too conservative of a solution that is not feasible for integration within the aircraft. Therefore, an overall system optimum is required wherein the transients and steady-state performance are optimized for such tightly-coupled systems. The intent of this effort is to establish an environment wherein detailed transient models of the various subsystems can be integrated to form an end-to-end system simulation. The environment must include DE devices such as solid state lasers and wide-band systems. System-level constraints include, but are not limited to, prime power, power conditioning, thermal management, and coupling apertures and antennas. System-level optimization techniques can then be applied with respect to power quality, size, weight, and thermal constraints. Trade studies can then be performed with respect to on-time, effectiveness, and range. The overall goal of the study consists of developing and demonstrating the necessary computational techniques to perfect a virtual prototype of a DE system on a representative airframe.
|| ||PHASE I: Define technical approach for an integrated directed energy system simulation and for system-level optimization. Demonstrate feasibility of this approach for a representative directed energy system.
|| || ||PHASE II: Design and develop system integration environment. Implement system-level optimization algorithms. Demonstrate capability for an airborne directed energy system.
|| ||DUAL USE COMMERCIALIZATION: Military application: Complete packaging of system integration and optimization software and implement using an airborne directed energy system. Commercial application: Complete packaging and system intergration for radio frequency sources.
|| References: ||1. C. E. Lucas, E. A. Walters, J. Jatskevich, O. Wasynczuk, P. T. Lamm, “A Distributed Heterogeneous Simulation of a Representative Aircraft Power System,” 2002 SAE Power Systems Conference Proceedings, October 2002, Coral Spring, Florida.
2. S. Graham, I. Wong, W. Chen, A. Lazarevic, K. Cleek, E. Walters, C. Lucas, O. Wasynczuk, P. Lamm, “Distributed Simulation,” Aerospace Engineering, pp. 24-27, November 2004.|
|Keywords: ||High Power Microwaves, High Power Lasers, Systems Integration|