Niching genetic algorithms-based characterization of geocentric orbits in the 3D elliptic restricted three-body problem

DOI10.1016/S0045-7825(02)00481-4zbMath1015.70011OpenAlexW2052422649MaRDI QIDQ1870994

Pini Gurfil, N. Jeremy Kasdin

Publication date: 6 May 2003

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7825(02)00481-4

zbMATH Keywords

trajectory optimizationgeocentric orbitsniching genetic algorithmsSun-Earth spatial elliptic restricted three-body problem

Mathematics Subject Classification ID

Three-body problems (70F07) Computational methods for problems pertaining to mechanics of particles and systems (70-08) Genetics and population dynamics (92D99)

Related Items (6)

A hybrid multiagent approach for global trajectory optimization ⋮ An improved nonlinear control strategy for deep space formation flying spacecraft ⋮ Long-term evolution of orbits about a precessing oblate planet: III: A semianalytical and a purely numerical approach ⋮ Hybrid Behavioral-Based Multiobjective Space Trajectory Optimization ⋮ Stability of two groups of multi-revolution elliptic halo orbits in the elliptic restricted three-body problem ⋮ Canonical modelling of relative spacecraft motion via epicyclic orbital elements

Cites Work

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• Solar sail parking in restricted three-body systems
• ON MOULTON'S ORBITS IN THE RESTRICTED PROBLEM OF THREE BODIES
• Introduction to Hamiltonian dynamical systems and the \(N\)-body problem
• Periodic solutions in the spatial elliptic restricted three-body problem

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