Octree-based reasonable-quality hexahedral mesh generation using a new set of refinement templates

  • Ito Y
  • Shih A
  • Soni B
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This paper presents an analytical model and a geometric numerical integrator for a tethered spacecraft model that is composed of two rigid bodies connected by an elastic tether. This model includes important dynamic characteristics of tethered spacecraft in orbit, namely the nonlinear coupling between tether deformations, rotational dynamics of rigid bodies, a reeling mechanism, and orbital dynamics. A geometric numerical integrator, referred to as a Lie group variational integrator, is developed to numerically preserve the Hamiltonian structure of the presented model and its Lie group configuration manifold. The structure-preserving properties are particularly useful for studying complex dynamics of a tethered spacecraft. These properties are illustrated by numerical simulations.

Author-supplied keywords

  • Biomedical applications
  • CSM
  • Grid generation
  • Mesh generation
  • Refinement templates
  • Unstructured hexahedral mesh

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  • Yasushi Ito

  • Alan M. Shih

  • Bharat K. Soni

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