Dynamics of earth-orbiting flexible satellites with multibody components
From MaRDI portal
Publication:3805998
DOI10.2514/3.20255zbMath0657.70028OpenAlexW2104741606MaRDI QIDQ3805998
Publication date: 1987
Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)
Full work available at URL: https://semanticscholar.org/paper/56b58641c75a85985f31155c0303bfe46473547f
inertial framerigid-body motionsConstraint conditionsdynamics of satellites with flexible multibody componentsrotationally-fixed floating frame
Related Items
Discrepancies of energy values in dynamics of three intersecting plates ⋮ Dynamics of sliding geometrically-exact beams: Large angle maneuver and parametric resonance ⋮ Stability of elastic rods with self-contact ⋮ Transient chaotic oscillations of a tethered satellite system ⋮ Modelling, dynamics and control of tethered satellite systems ⋮ An energy conserving numerical scheme for the dynamics of hyperelastic rods ⋮ Self-contact modeling on beams experiencing loop formation ⋮ Multibody Dynamics and Nonlinear Control of Flexible Space Structures ⋮ Dynamics of 3D sliding beams undergoing large overall motions ⋮ A computational procedure for interaction of high-speed vehicles on flexible structures without assuming known vehicle nominal motion ⋮ A co-rotational formulation for 3D beam element using vectorial rotational variables ⋮ Tethered satellite systems: A challenge for mechanics and applied mathematics ⋮ A general formulation for the nonlinear dynamics and control of orbiting flexible structures
This page was built for publication: Dynamics of earth-orbiting flexible satellites with multibody components
