Upcoming! February 20, 2026, Friday, 03:00PM (GMT+03.00, Moscow), IKI, Room 200
Abstract:
The work is devoted to the development of the methods for studying the trajectories of multi-orbit low-thrust transfers. A
mathematical model of the averaged orbital motion of a spacecraft with low thrust is proposed.
Approximate solutions for the evolution of a nearly circular orbit under periodic perturbative acceleration are obtained.
Based on the averaged model, a new methodology to obtain optimal multi-turn orbital transfers is developed.
The presented methodology is applied in a preliminary ballistic analysis of a promising mission to study the Earth magnetosphere
(based on a PhD dissertation)