Lissajous and halo orbits in the restricted three-body problem by normalization method-Reference-Cited by-同舟云学术

Lissajous and halo orbits in the restricted three-body problem by normalization method

Published:2020-08-11 Issue:4 Volume:101 Page:2629-2644
ISSN:0924-090X
Container-title:Nonlinear Dynamics
language:en
Short-container-title:Nonlinear Dyn

Author:

Luo Tong,Pucacco Giuseppe,Xu Ming^ORCID

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Ministry of Education of China

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s11071-020-05875-1.pdf

Reference27 articles.

1. Brouwer, D., Clemence, G.M.: Methods of Celestial Mechanics. Academic Press, New York (1961)

2. Meyer, K.R., Hall, G.R.: Introduction to Hamiltonian Dynamical Systems and the N-Body Problem. Springer, New York (1991)

3. Henrard, J.: Periodic orbits emanating from a resonant equilibrium. Celest. Mech. 1(3–4), 427–466 (1970)

4. Pucacco, G., Marchesiello, A.: An energy-momentum map for the time-reversal symmetric 1:1 resonance with Z2 × Z2 symmetry. Physica D 271, 10–18 (2014)

5. Farquhar, R.W.: The utilization of halo orbits in advanced lunar operations. NASA technical note. NASA TN D-6365 (1971)

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