Mathematical modelling and stabilization of large flexible spacecraft subject to orbital perturbation

DOI10.1016/0895-7177(89)90326-9zbMath0697.70026OpenAlexW2070523362MaRDI QIDQ911825

N. E. Zubov

Publication date: 1989

Published in: Mathematical and Computer Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0895-7177(89)90326-9

zbMATH Keywords

Hamilton's principleLyapunov's approachmodelling of large flexible spacecraftstabilization under the influence of orbital (radial) perturbation

Mathematics Subject Classification ID

Control of mechanical systems (70Q05) Nonlinear dynamics in mechanics (70K99) Orbital mechanics (70M20)

Related Items (1)

Stability and robustness analysis of boundary control of a flexible space structure

Cites Work

• Unnamed Item
• Stabilization of a class of hybrid systems arising in flexible spacecraft
• Mathematical modeling and control of large space structures with multiple appendages
• Modelling of flexible spacecraft and their stabilization†
• Stability of flexible spacecrafts
• Hamilton's principle - Finite-element methods and flexible body dynamics
• Long-term coupling effects between librational and orbital motions of a satellite

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