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Parallel Design Tools for Optimization of Smart Structures

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: DASG60-03-C-0004
Agency Tracking Number: 99-558
Amount: $807,349.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: BMDO99-012
Solicitation Number: 1999.1
Timeline
Solicitation Year: 1999
Award Year: 2004
Award Start Date (Proposal Award Date): 2003-02-17
Award End Date (Contract End Date): 2005-02-17
Small Business Information
6508 Anna Maria Court
McLean, VA 22101
United States
DUNS: 046772211
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: Yes
Principal Investigator
 Rong Shieh
 Chief Scientist
 (703) 356-0122
 shieh@mhpcc.edu
Business Contact
 Rong Shieh
Title: President
Phone: (703) 356-0122
Email: shieh@mhpcc.edu
Research Institution
N/A
Abstract

This SBIR Phase II project is to continuously and fully develop the title parallel computational design tools initiated in Phase I into superpowerful, commercializable prototype design tools (computer codes) in the following manner: (i) adopting/extending our own superefficient Integral Global/Local Optimization (IGLO) algorithms, (ii) extending/developing some efficient constraint treatment schemes, (iii) using smart structural (active element placement) technology to significantly improve the global minimum solution result, (iv) adopting/developing some efficient parallel computational optimization and finite element structural analysis methods, (v) adopting and parallelizing a multi-objective optimization method, and (vi) combining the above algorithms/schemes/methods into superpowerful parallel computerized smart structural design analysis and optimization technology. These tools consist of the IGLOAP (IGLO Algorithm Package), PASA (Parallel Adaptive Structural Analyzer), and PASOS (Parallel Adaptive Structural Optimization System) codes. Development of these tools are particular important in significantly improving the design efficiency/cycle time and quality (global minimum solution value) of structures and hardware systems, including weapon-carrying, aerospace-borne precision structures for ballistic missile defense use, for which minimum structural weight and/or minimum pointing error design(s) is (are) of primary importance. In particular, it enables solution of unprecedentedly large-size structural design problems with mixed-discrete/continuous design variables without incurring excessive computational time/cost.

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

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