Minimum-Energy Transfer Optimization between Near-Circular Orbits Using an Approximate Closed-Form Solution
This paper explores the use of the averaging method in the optimal control problem related to the multirevolution orbital transfer of a spacecraft with low-thrust capabilities. The regularized equations of motion are expressed using modified equinoctial elements with the eccentric longitude as a fas...
Main Authors: | Kirill Suslov, Maksim Shirobokov, Anastasia Tselousova |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-11-01
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Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/12/1002 |
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