Email this article Existence Domain for Solutions of Optimal Control Problems for Bounded-Thrust Spacecrafts
- Authors: Ivanyukhin A.V.1,2
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Affiliations:
- State Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)
- RUDN University
- Issue: Vol 239, No 6 (2019)
- Pages: 817-839
- Section: Article
- URL: https://journal-vniispk.ru/1072-3374/article/view/242708
- DOI: https://doi.org/10.1007/s10958-019-04328-4
- ID: 242708
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Abstract
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.
About the authors
A. V. Ivanyukhin
State Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University); RUDN University
Author for correspondence.
Email: ivanyukhin.a@yandex.ru
Russian Federation, Moscow; Moscow
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