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Optimal Multi-impulse Elliptic Rendezvous Using Stagnation Escaping Whale Optimization AlgorithmOptimal Multi-impulse Elliptic Rendezvous Using Stagnation Escaping Whale Optimization Algorithm

Other Titles
Optimal Multi-impulse Elliptic Rendezvous Using Stagnation Escaping Whale Optimization Algorithm
Authors
심은송김해동이선호
Issue Date
Jul-2024
Publisher
The Korean Society for Aeronautical & Space Sciences
Keywords
multi-impulse elliptic rendezvous; stagnation escaping whale optimization algorithm (SE WOA); adaptive balancing paramet
Citation
International Journal of Aeronautical and Space Sciences, v.25, no.3, pp 1092 - 1104
Pages
13
Indexed
SCIE
SCOPUS
KCI
Journal Title
International Journal of Aeronautical and Space Sciences
Volume
25
Number
3
Start Page
1092
End Page
1104
URI
https://scholarworks.gnu.ac.kr/handle/sw.gnu/71538
DOI
10.1007/s42405-024-00713-9
ISSN
2093-274X
2093-2480
Abstract
Various optimization algorithms have been applied to obtain a global solution for rendezvous trajectory optimization problems. However, the global solution is not always ensured due to performance limitations of the optimization algorithms. In this paper, we investigate the optimal fuel consumption multi-impulse elliptic rendezvous using stagnation escaping whale optimization algorithm (SE-WOA). We construct a mathematical model of the elliptic rendezvous based on Tschauner–Hempel equations and an optimization model including practical constraints to describe a practical rendezvous. We propose the SE-WOA which has strong global search ability and fast convergence speed with an adaptive balancing parameter. A case study of three-impulse rendezvous is performed to verify improvements using SE-WOA and compare the result of the SE-WOA with other optimization algorithms.
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