Optimizing the Support of a Stellar Sensor
- Authors: Novokshenov A.D.1, Marchenko P.A.1, Nemov A.S.1, Borovkov A.I.1
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Affiliations:
- Peter the Great St. Petersburg Polytechnic University
- Issue: Vol 38, No 1 (2018)
- Pages: 7-12
- Section: Article
- URL: https://journal-vniispk.ru/1068-798X/article/view/227362
- DOI: https://doi.org/10.3103/S1068798X18010148
- ID: 227362
Cite item
Abstract
The mass of a support for a stellar sensor in a spacecraft is minimized in the light of requirements on the first eigenfrequency and the reactive force in the connectors. Topological and parametric optimization is employed. The finite-element method is adopted, within the capabilities of the Altair Optistruct system
About the authors
A. D. Novokshenov
Peter the Great St. Petersburg Polytechnic University
Author for correspondence.
Email: novokshenov@compmechlab.com
Russian Federation, St. Petersburg
P. A. Marchenko
Peter the Great St. Petersburg Polytechnic University
Email: novokshenov@compmechlab.com
Russian Federation, St. Petersburg
A. S. Nemov
Peter the Great St. Petersburg Polytechnic University
Email: novokshenov@compmechlab.com
Russian Federation, St. Petersburg
A. I. Borovkov
Peter the Great St. Petersburg Polytechnic University
Email: novokshenov@compmechlab.com
Russian Federation, St. Petersburg
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