June 26 - 30, 2004
Saturday to Wednesday
Seattle, Washington, USA

 

 

Session:

EVH - Application of Hybrid Evolutionary Algorithms to Complex Optimization Problems

Title:

Application of a New Hybrid Evolutionary Strategy to Spacecraft Thermal Design

   

Authors:

Roberto L. Galski
Fabiano L. Sousa
Fernando M. Ramos
Issamu Muraoka

   

Abstract:

In this paper, a new hybrid evolutionary strategy is used to the inverse design of a spacecraft thermal control system. This hybrid strategy comprises one step of global, stochastic search, using the Generalized Extremal Optimization (GEO) algorithm, followed by a local, deterministic refinement minimization step with the EXTREM optimization routine. The GEO algorithm is a novel global search meta-heuristic, based on a model of natural evolution, while EXTREM uses Powell’s method of conjugate directions. This approach is applied to the inverse design of a spacecraft thermal control system, considering different critical, on-orbit operational conditions. Numerical results show that the hybrid approach improves the design solution in terms of the value of the objective function, while GEO yields non-intuitive efficient solutions in the sense they were unlikely to come out through the classical, “manual” design procedure.

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