Design Optimization of Space Debris Decent Trajectory Considering Land Security by Evolutionary Calculation
Author:
Affiliation:
1. Graduate School of System Design, Tokyo Metropolitan University
Publisher
Japan Society for Fuzzy Theory and Intelligent Informatics
Subject
General Medicine
Link
https://www.jstage.jst.go.jp/article/jsoft/35/1/35_571/_pdf
Reference12 articles.
1. [1] C. Bombardelli and J. Pelaez: “Ion Beam Shepherd for Contactless Space Debris Removal,” J. of Guidance, Control, and Dynamics, Vol.34, No.3, pp. 916-920, 2011.
2. [2] S. I. Nishida, S. Kawamoto, Y. Okawa, F. Terui, and S. Kitamura: “Space debris removal system using a small satellite,” Acta Astronautica, Vol.65, No.1, pp. 95-102, 2009.
3. [3] C. P. Mark and D. Kamath: “Review of Active Space Debris Removal Methods,” Space Policy, Vol.47, pp. 194-206, 2019.
4. [4] Y. Chen, Y. Bai, Y. Zhao, Y. Wang, and X. Chen: “Optimal mission planning of active space debris removal based on genetic algorithm,” IOP Conf. Series: Materials Science and Engineering, Vol.715, No.1, 012025, 2020.
5. [5] M. Kanazaki, Y. Yamada, and M. Nakamiya: “Trajectory optimization of a satellite for multiple active space debris removal based on a method for the traveling serviceman problem,” 21st Asia Pacific Symp. on Intelligent and Evolutionary Systems (IES), pp. 61-66, 2017.
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