Earth-Mars halo to halo low thrust manifold transfers

DOI10.1007/s10569-009-9205-6zbMath1223.70093OpenAlexW1975243902MaRDI QIDQ642292

C. Casaregola, P. Pergola, K. Geurts, M. Andrenucci

Publication date: 26 October 2011

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-009-9205-6

zbMATH Keywords

halo orbitsbicircular modelcircular restricted three body problemEarth-to-Mars transferslow thrustlow-thrust manifolds

Mathematics Subject Classification ID

Three-body problems (70F07) Orbital mechanics (70M20)

Related Items (6)

Earth-Mars transfers with ballistic escape and low-thrust capture ⋮ A multi-objective approach to the design of low thrust space trajectories using optimal control ⋮ Using space manifold dynamics to deploy a small satellite constellation around the Moon ⋮ The use of invariant manifolds for transfers between unstable periodic orbits of different energies ⋮ Transfers between libration point orbits of Sun-Earth and Earth-Moon systems by using invariant manifolds ⋮ High-order solutions around triangular libration points in the elliptic restricted three-body problem and applications to low energy transfers

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• Three-Body Invariant Manifold Transition with Electric Propulsion
• Survey of Numerical Methods for Trajectory Optimization
• Analytic construction of periodic orbits about the collinear points
• BURRAU'S PROBLEM OF THREE BODIES

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