Paper Title:
Engineering Applications of Satellite Structural Optimization Utilizing ANSYS/CATIA
  Abstract

A structured frame for the design optimization problem of satellite platform structure was established through the definition, flow and modification research of design parameters in the ANSYS/CATIA system. Problems with creating complex satellite structure FEA (Finite Element Analysis) models were discussed, including the idealization of real structure, as well as embedment of APDL (ANSYS Parametric Design Language) programme developed specially for the pre-processing and post-processing of FEA model. The optimization model was established under structural design requirements, and a graded optimization method was applied for calculation. Light-weight design schemes for two satellite platform structure were obtained through the subsequently optimization implemented using approaches put forward previously. The optimization design problems of two satellite platform structure were settled well, and work done in this paper provides certain reference value for optimization of other spacecraft structures.

  Info
Periodical
Chapter
Chapter 8: Machining
Edited by
Wu Fan
Pages
1567-1575
DOI
10.4028/www.scientific.net/AMM.110-116.1567
Citation
J. Mao, W. H. Zhang, "Engineering Applications of Satellite Structural Optimization Utilizing ANSYS/CATIA", Applied Mechanics and Materials, Vols. 110-116, pp. 1567-1575, 2012
Online since
October 2011
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Price
$32.00
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