Optimizing the Support of a Stellar Sensor


Cite item

Full Text

Open Access Open Access
Restricted Access Access granted
Restricted Access Subscription Access

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

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2018 Allerton Press, Inc.