Forming the conceptual structure of a dimensionally stable platform by numerical optimization

Abstract


The paper presents a problem of adjusting the dynamic characteristics of a space vehicle that emerges in the course of restructuring its dimensionally stable structure. The adjustment is accomplished with the help of numerical optimization. The response of the structure is modeled by the finite element method.


About the authors

K. V. Peresypkin

Samara State Aerospace University

Author for correspondence.
Email: peresypkin_kv@mail.ru

Russian Federation

Assistant of Aircraft Design Department

M. S. Kozhichenkova

Space Rocket Center “TsSKB-Progress”, Samara

Email: bellana1588@mail.ru

Russian Federation

Design Engineer

References

  1. Gregory, J. Moore, MSC/NASTRAN Version 68 Design Sensitivity and Optimization User`s Guide, The MacNeal-Schwendler Corporation, 1994.

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