A problem of relative motion of orbiting bodies is investigated on the example of the free motion of any body ejected from the orbital station that stays in a circular orbit around the earth. An elementary approach is illustrated by a simulation computer program and supported by a mathematical treatment based on approximate differential equations of the relative orbital motion. 1. Relative moti...

The relative motion of an outline the rendezvous problem has been studied by assuming that chief satellite is in circular symmetric orbits. legitimacy perturbation techniques and nonlinear are investigated. deputy equations with respect to fixed references at center general case. We found periodic solutions linear for using Lindstedt–Poincaré technique. Comparisons among analytical motions obta...