Periodic Solutions of Nonlinear Relative Motion Satellites

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 obtained solution numerical integration explicit Euler method both demonstrate periodic. However, technique non-periodic. Thus, recommended designing solutions. Furthermore, a comparison between investigated graphically.