Minimum-Energy Transfer Optimization between Near-Circular Orbits Using an Approximate Closed-Form Solution

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...

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Bibliographic Details
Main Authors: Kirill Suslov, Maksim Shirobokov, Anastasia Tselousova
Format: Article
Language:English
Published: MDPI AG 2023-11-01
Series:Aerospace
Subjects:
orbital transfer
approximate solution
close form
trajectory optimization
low thrust
Online Access:https://www.mdpi.com/2226-4310/10/12/1002

Internet

https://www.mdpi.com/2226-4310/10/12/1002

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