Trajectory optimization of space vehicle in rendezvous proximity operation with evolutionary feasibility conserving techniques

In this paper, a direct approach is developed for discovering optimal transfer trajectories of close-range rendezvous of satellites considering disturbances in elliptical orbits. The control vector representing the inputs is parameterized via different interpolation methods, and an Estimation of Dis...

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Bibliographic Details
Published in:Engineering applications of artificial intelligence Vol. 117; p. 105523
Main Authors: Shirazi, Abolfazl, Ceberio, Josu, Lozano, Jose A.
Format: Journal Article
Language:English
Published: Elsevier Ltd 01.01.2023
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ISSN:0952-1976, 1873-6769
Online Access:Get full text
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