Output regulation of a flexible spacecraft with exponentially stable/unstable internal dynamics

DOI10.1016/S0947-3580(98)70110-4zbMath0913.93049OpenAlexW1980870395MaRDI QIDQ1267267

Pasquale Lucibello

Publication date: 7 June 1999

Published in: European Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0947-3580(98)70110-4

zbMATH Keywords

flexible spacecraftoutput trackingattitudesnonlinear regulationunstable internal dynamics

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Nonlinear systems in control theory (93C10) Application models in control theory (93C95)

Related Items (1)

State steering by learning for a class of nonlinear control systems

Cites Work

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• A balanced LQG compensator for flexible structures
• Output regulation of nonlinear systems evolving in the neighborhood of a periodic orbit
• An introduction to continuum mechanics
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• Dynamics of Flexible Bodies Using Generalized Newton-Euler Equations
• Output regulation of nonlinear systems
• Inversion techniques for trajectory control of flexible robot arms
• Decomposition techniques for large-scale systems with nonadditive interactions: Stability and stabilizability
• A finite element approach to kinetic energy discretization of deformable bodies in quasi‐rigid motion
• A note on a necessary condition for output regulation
• Component model reduction methodology for articulate multiflexible body structures

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