Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations

DOI10.1134/S0005117909070030zbMath1181.93038MaRDI QIDQ1040489

V. M. Sukhanov, I. N. Krutova

Publication date: 24 November 2009

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

zbMATH Keywords

mathematical modelingelastic oscillationsnonlinear orientation control systemvariation of the boundaries of the stability domains

Mathematics Subject Classification ID

Nonlinear systems in control theory (93C10) Design techniques (robust design, computer-aided design, etc.) (93B51) Discrete-time control/observation systems (93C55) Adaptive or robust stabilization (93D21) Robust stability (93D09) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (1)

Angular motion control of a large space structure with elastic elements

Cites Work

• Methods of intelligent diagnosis for control of flexible moving craft
• Design of modified PD algorithm to control angular motion of large space structure
• Studying stability of the flexible spacecraft with a discrete control system
• Spatial angular motion of a flexible spacecraft: the modal-physical model and its characteristics
• Dynamics and control of large space structures

This page was built for publication: Design of discrete control system of flexible spacecraft maintaining robust stability of elastic oscillations