Efficient invariant-manifold, low-thrust planar trajectories to the Moon-Reference-Cited by-同舟云学术

Efficient invariant-manifold, low-thrust planar trajectories to the Moon

Published:2012-02 Issue:2 Volume:17 Page:817-831
ISSN:1007-5704
Container-title:Communications in Nonlinear Science and Numerical Simulation
language:en
Short-container-title:Communications in Nonlinear Science and Numerical Simulation

Author:

Mingotti G.,Topputo F.,Bernelli-Zazzera F.

Publisher

Elsevier BV

Subject

Applied Mathematics,Modelling and Simulation,Numerical Analysis

Reference22 articles.

1. Sun-perturbed Earth-to-Moon transfers with ballistic capture;Belbruno;J Guidance Contr Dyn,1993

2. Belbruno EA. The dynamical mechanism of ballistic lunar capture transfers in the four-body problem from the perspective of invariant manifolds and Hill’S regions. Barcelona, Spain, 1994.

3. Low energy transfer to the Moon;Koon;Celest Mech Dyn Astron,2001

4. Invariant manifolds, the spatial three-body problem, and space mission design;Gómez;Adv Astronaut Sci,2001

5. Shoot the Moon 3D;Parker;Adv Astronaut Sci,2006

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