Numerical Determination of Short Period Trojan Orbits in the Restricted Three Body Problem
1965
27 pages
Report
No indication
English
Spacecraft Trajectories & Flight Mechanics , Libration , Orbital calculation , Three-body problem , Body , Calculation , Eccentricity , Ellipse , Jacobi integral , Linear , Mass , Orbital , Period , Plane , Point , Problem , Short , Stability , Three
Quasi‐Periodic Orbits of the Restricted Three‐Body Problem Made Easy
American Institute of Physics | 2007
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