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

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. © 2019, Springer Science+Business Media, LLC, part of Springer Nature.

Authors
Publisher
Springer New York LLC
Number of issue
6
Language
English
Pages
817-839
Status
Published
Volume
239
Year
2019
Organizations
  • 1 State Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University), Moscow, Russian Federation
  • 2 RUDN University, Moscow, Russian Federation
Date of creation
19.07.2019
Date of change
19.07.2019
Short link
https://repository.rudn.ru/en/records/article/record/38559/