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Methods of estimating the envelope of elastic oscillations of the flexible spacecraft

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Publication:1778643
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DOI10.1023/A:1015126114663zbMath1116.74408OpenAlexW1543370319MaRDI QIDQ1778643

A. V. Silaev, V. M. Sukhanov

Publication date: 17 June 2005

Published in: Automation and Remote Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1015126114663



Mathematics Subject Classification ID

Elastic materials (74B99) Homogenization and oscillations in dynamical problems of solid mechanics (74Q10)


Related Items (3)

Parametric adaptation algorithm for the basic law used to control orientation of a large space structure on the base of flexible modes envelope estimation ⋮ Adaptive approach with the ``fast model for dynamics identification and forecasting problems for relay control of an elastic satellite ⋮ Some questions of control of the robotized in-orbit assembly of large space structures







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