The Theory of Long-Term Behavior of Artificial Satellite Orbits Due to Third-Body Perturbations
1966
53 pages
Report
Keine Angabe
Englisch
Spacecraft Trajectories & Flight Mechanics , Elliptic integral , Nonlinear equation , Satellite , Satellite perturbation , Three-body problem , Angle , Average , Body , Ellipse , Equation , Integral , Lunar , Motion , Node , Nonlinear , Orbit , Periodic , Perturbation , Problem , Three
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