On the practical stability of the triangular points in the restricted three-body problem Jacek Olszewski OriginalPaper Pages: 3 - 14
Periodic, consecutive-collision orbits in the restricted problem forμ≠1/2 E. Myles Standish Jr. OriginalPaper Pages: 31 - 43
Sufficient conditions for escape in the three-body problem E. Myles Standish Jr. OriginalPaper Pages: 44 - 48
On the integrability cases of the equation of motion for a satellite in an axially symmetric gravitational field Abolghassem Ghaffari OriginalPaper Pages: 49 - 53
Stability of and motion aboutL 4 at three-to-one commensurability K. T. Alfriend OriginalPaper Pages: 60 - 77
Attitude stability of a symmetric satellite at the equilibrium points in the restricted three-body problem T. R. KaneE. L. Marsh OriginalPaper Pages: 78 - 90
Periodic orbits near ℒ4 for mass ratios near the critical mass ratio of routh K. R. MeyerD. S. Schmidt OriginalPaper Pages: 99 - 109
Classification of the motions of three bodies in a plane Victor Szebehely BriefCommunication Pages: 116 - 118
A note on ‘The main problem of satellite theory for small eccentricities, by A. Deprit and A. Rom, 1970’ Kaare Aksnes OriginalPaper Pages: 119 - 121
