The effect of orbital eccentricity and nodal regression on spin-stabilized satellites Vladimir N. DvornychenkoR. Bruce Gerding OriginalPaper Pages: 263 - 274
Second species solutions with an 0(μν), 1/3<ν<1, near-moon passage L. M. Perko OriginalPaper Pages: 275 - 290
Operational requirements and the geometry of a station-keeping maneuver J. B. Eades Jr. OriginalPaper Pages: 315 - 342
An element formulation for perturbed motion about the center of mass John D. DonaldsonDonald J. Jezewski OriginalPaper Pages: 367 - 387
