Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations

DOI10.1134/S0005117908060040zbMath1156.93031MaRDI QIDQ1002975

A. S. Ermilov, V. M. Sukhanov, V. Yu. Rutkovskii, T. V. Ermilova

Publication date: 26 February 2009

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

zbMATH Keywords

flexible objectselastic oscillationsKalman estimation

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Application models in control theory (93C95) Nonlinear elasticity (74B20) Stochastic systems in control theory (general) (93E03)

Related Items (4)

Estimating nonmeasurable coordinates of elastic oscillations for large space constructions with a gyroforce engine ⋮ Nonlinear control with distributed delay for the angular stabilization of a rigid body ⋮ Methods for the vibration determination and parameter identification of spacecraft with flexible structures ⋮ Synthesis of an active compensation algorithm for elastic oscillations with nonstationary parameters for deformable spacecrafts

Cites Work

• Control of the angular motion of a semiactive bundle of bodies relying on the estimates of nonmeasurable coordinated obtained by Kalman filtering methods
• Unnamed Item

This page was built for publication: Two-level orientation control system of flexible spacecraft with active stabilization of structural elastic oscillations