Three-dimensional motion of a large flexible satellite

DOI10.1016/0005-1098(72)90047-7zbMath0251.70015OpenAlexW2031222989MaRDI QIDQ2557135

Corrado Poli, Richard Budynas

Publication date: 1972

Published in: Automatica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0005-1098(72)90047-7

Mathematics Subject Classification ID

Hamilton's equations (70H05) Orbital mechanics (70M20)

Related Items (1)

On some attitude control syntheses for satellites with flexible appendages

Cites Work

• Unnamed Item
• Stability analysis of elastic and aeroelastic systems via Lyapunov's direct method
• Dynamics of an elastic satellite. II
• On dynamic stability of elastic bodies with prescribed initial conditions
• The direct method of Liapunov in stability problems of elastic systems
• On the effect of aerodynamic and gravitational torques on the attitude stability of satellites.
• Stability of the force-free motions of a dual- spin spacecraft.
• Stability of a spinning body containing elastic parts via Liapunov'sdirect method
• On the stability of a body with connected moving parts.
• Planar Motion of a Large Flexible Satellite
• Asymptotic stability and instability criteria for some elastic systems by Liapunov’s direct method

This page was built for publication: Three-dimensional motion of a large flexible satellite