A general formulation for librational dynamics of spacecraft with deploying appendages

DOI10.2514/3.19895zbMath0567.70029OpenAlexW2092993427MaRDI QIDQ3683595

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Publication date: 1984

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.19895

zbMATH Keywords

attitude dynamicseffect of flexibility and deploymentflexible satellite systemsgeneral set of librational equationsgeneralised librational dynamicsstability of spacecrafts

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Composite and mixture properties (74E30) Astronomy and astrophysics (85A99) Orbital mechanics (70M20)

Related Items (6)

A Class of Novel Space Platform-Based Manipulators With Slewing and Deployable Links: Analyses and Experiments ⋮ Integrated vibration suppression attitude control for flexible spacecrafts with internal liquid sloshing ⋮ Multibody Dynamics and Nonlinear Control of Flexible Space Structures ⋮ On the coupled dynamics of small spacecraft and elastic deployable appendages ⋮ Stability analysis of nonlinear vibrations of a deploying flexible beam ⋮ A general formulation for the nonlinear dynamics and control of orbiting flexible structures

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