G.G. Bulychev1, V.B. Fedorov2

1,2 MIREA – Russian University of Technology (Moscow, Russia)
1 geo-bulychev@mail.ru, 2 fdorov@mail.ru

The divergence of satellite trajectories during multiple maneuvers is investigated.

Goal – to show that common three-dimensional relative orbits and non-centered periodic orbits can be locally observable, assuming that the system with the upgraded Kalman filter will continue to track the corresponding trajectory after the filter is activated.

The jumps of the travelers' orbit during its perturbation are described, which made it possible to divide the orbits into stationary (inertial) sections and perturbations.

The classes of possible orbits in the case of a brief satellite maneuver are determined, and the possibility of such orbits drifting is shown.

Bulychev G.G., Fedorov V.B. Divergence of relative satellite trajectories during a short maneuver. Achievements of modern radioelectronics. 2025. V. 79. № 12. P. 24–31. DOI: https://doi.org/10.18127/ j20700784-202512-05 [in Russian]

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