Using the method of phase biplane to study dynamics of interactions of the elastic structural oscillations of the flexible spacecraft with the control system

DOI10.1134/S0005117907020063zbMath1126.93042OpenAlexW2064481309MaRDI QIDQ2371583

V. M. Sukhanov, V. Yu. Rutkovskii

Publication date: 5 July 2007

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

Full work available at URL: https://doi.org/10.1134/s0005117907020063

zbMATH Keywords

stabilitymathematical modelcontrol of flexible spacecraftstructural oscillations

Mathematics Subject Classification ID

Application models in control theory (93C95) Linear systems in control theory (93C05) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• Spatial angular motion of a flexible spacecraft: the modal-physical model and its characteristics

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