Existence Domain for Solutions of Optimal Control Problems for Bounded-Thrust Spacecrafts


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We consider several of the most common optimal-control problems for low-thrust spacecrafts. We investigate the existence of solutions for those problems. For the bounded-thrust model, we use the numerical approach to construct the existence domain. As examples, we consider the Earth–Mars and Earth–Mercury interplanetary flights.

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A. Ivanyukhin

State Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University); RUDN University

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Email: ivanyukhin.a@yandex.ru
俄罗斯联邦, Moscow; Moscow

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