Mathematical modeling and control of large space structures with multiple appendages

DOI10.1016/0895-7177(88)90181-1zbMath0656.70032OpenAlexW1976964627MaRDI QIDQ1110365

S. H. Smith

Publication date: 1988

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

Full work available at URL: https://doi.org/10.1016/0895-7177(88)90181-1

zbMATH Keywords

modelingasymptotically stablefeedback control schemesstabilization of large satellites with several flexible appendages

Mathematics Subject Classification ID

Controllability (93B05) Control/observation systems governed by partial differential equations (93C20) Control of mechanical systems (70Q05) Orbital mechanics (70M20)

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Existence of solutions to strongly damped plate or beam equations ⋮ Mathematical modelling and stabilization of large flexible spacecraft subject to orbital perturbation ⋮ On the vibrations of a simply supported square plate on a weakly nonlinear elastic foundation ⋮ On aspects of asymptotics for plate equations

Cites Work

• Stabilization of a class of hybrid systems arising in flexible spacecraft
• Modelling of flexible spacecraft and their stabilization†
• Attitude Control of a Flexible Spacecraft
• Robust colocated control for large flexible space structures
• Trends in large space structure control theory: Fondest hopes, wildest dreams
• Stability of a spinning body containing elastic parts via Liapunov'sdirect method
• A Method for the Liapunov Stability Analysis of Force-Free Dynamical Systems