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Forming the conceptual structure of a dimensionally stable platform by numerical optimization
- Authors: Peresypkin K.V.1, Kozhichenkova M.S.2
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Affiliations:
- Samara State Aerospace University
- Space Rocket Center “TsSKB-Progress”, Samara
- Issue: Vol 12, No 4 (2013)
- Pages: 223-230
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/44
- DOI: https://doi.org/10.18287/1998-6629-2013-0-4(42)-223-230
- ID: 44
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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
Assistant of Aircraft Design Department
Russian FederationM. S. Kozhichenkova
Space Rocket Center “TsSKB-Progress”, Samara
Email: bellana1588@mail.ru
Design Engineer
Russian FederationReferences
- Gregory, J. Moore, MSC/NASTRAN Version 68 Design Sensitivity and Optimization User`s Guide, The MacNeal-Schwendler Corporation, 1994.
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