Genetic Algorithm Applied to Design Knowledge Discovery of Launch Vehicle Using Clustered Hybrid Rocket
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-89988-6_31
Reference8 articles.
1. Deb, K., Pratap, A., Agarwal, S., Meyarivan, T.: A fast and elitist multiobjective genetic algorithm: NSGA-II. IEEE Trans. Evol. Comput. 6(2), 182–197 (2002)
2. Eshelman, L., Schaffer, J.: Real-Coded Genetic Algorithms and Interval-Schemata, pp. 187–202 (1993)
3. Hikone, S.: Regression Rate Characteristics and Combustion Mechanism of Some Hybrid Rocket Fuels (2010)
4. Kanazaki, M., Kanamori, F., Kitagawa, Y., Nakamiya, M., Kitagawa, K., Shimada, T.: Conceptual design: dependence of parameterization on design performance of three-stage hybrid rocket. Trans. Jpn. Soc. Aeronaut. Sp. Sci. 9 (2014)
5. Kitagawa, Y., Kitagawa, K., Nakamiya, M., Kanazaki, M., Shimada, T.: Multi-stage hybrid rocket conceptual design for mi-cro-satellites launch using genetic algorithm. Trans. Jpn. Soc. Aeronaut. Sp. Sci. 55(4), 229–236 (2012)
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