The stability of second species periodic orbits in the restricted problem (μ = 0)

Author:

Hitzl Donald L.,Hénon Michel

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference15 articles.

1. Periodic solutions of the restricted three body problem representing analytic continuations of Keplerian elliptic motions;Arenstorf;Amer. J. Math.,1963

2. Periodic trajectories passing near both masses of the restricted three-body problem;Arenstorf,1963

3. Matched asymptotic expansions, patched conics, and the computation of interplanetary trajectories;Breakwell,1966

4. Second-order matching in the restricted three-body problem (small μ);Breakwell;Celes. Mech.,1974

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