Marshall Technical Reports Server

Evolutionary Optimization of a Geometrically Refined Truss

NASA/TP—2007–214960, Hull, P.V. and Tinker, M.L. and Dozier, G.V., Evolutionary Optimization of a Geometrically Refined Truss, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812, National Aeronautics and Space Administration, Washington, DC 20546–0001, June 2007, pp. 32, Format(s): PDF 11129k

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this area have developed optimization tools to successfully design and model structures, typically minimizing mass while maintaining certain deflection and stress constraints. Numerous optimization studies have been performed to minimize mass, deflection, and stress on a benchmark cantilever truss problem. Predominantly traditional optimization theory is applied to this problem. The cross-sectional area of each member is optimized to minimize the aforementioned objectives. This Technical Publication (TP) presents a structural optimization technique that has been previously applied to compliant mechanism design. This technique demonstrates a method that combines topology optimization, geometric refinement, finite element analysis, and two forms of evolutionary computation: genetic algorithms and differential evolution to successfully optimize a benchmark structural optimization problem. A nontraditional solution to the benchmark problem is presented in this TP, specifically a geometrically refined topological solution. The design process begins with an alternate control mesh formulation, multilevel geometric smoothing operation, and an elastostatic structural analysis. The design process is wrapped in an evolutionary computing optimization toolset.
Keywords:subdivision, elastostatic, topology, optimization, genetic algorithms
Subjects:Engineering: Structural Mechanics
ID Code:750
Deposited On:23 July 2007