THE PERTURBATIONS OF SATELLITE ORBITS BY THE GRAVITATIONAL EFFECTS OF AN EXTERNAL BODY.
NAVAL WEAPONS LAB DAHLGREN VA
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An outline is given of the method used in the determination of Luni-solar perturbations on an artificial satellite of an oblate Earth without atmosphere. The first order theory was completed and a scheme for the evaluation of a second order theory is presented. Author
- Spacecraft Trajectories and Reentry