Performance of Gradient-Based Solutions versus Genetic Algorithms in the Correlation of Thermal Mathematical Models of Spacecrafts
dc.contributor.author | Anglada, Eva | |
dc.contributor.author | Martinez-Jimenez, Laura | |
dc.contributor.author | Garmendia, IƱaki | |
dc.contributor.institution | CIRMETAL | |
dc.date.issued | 2017-05-24 | |
dc.description | Publisher Copyright: Ā© 2017 Eva Anglada et al. | |
dc.description.abstract | The correlation of the thermal mathematical models (TMMs) of spacecrafts with the results of the thermal test is a demanding task in terms of time and effort. Theoretically, it can be automatized by means of optimization techniques, although this is a challenging task. Previous studies have shown the ability of genetic algorithms to perform this task in several cases, although some limitations have been detected. In addition, gradient-based methods, although also presenting some limitations, have provided good solutions in other technical fields. For this reason, the performance of genetic algorithms and gradient-based methods in the correlation of TMMs is discussed in this paper to compare the pros and cons of them. The case of study used in the comparison is a real space instrument flown on board the International Space Station. | en |
dc.description.status | Peer reviewed | |
dc.format.extent | 12 | |
dc.format.extent | 2586198 | |
dc.identifier.citation | Anglada , E , Martinez-Jimenez , L & Garmendia , I 2017 , ' Performance of Gradient-Based Solutions versus Genetic Algorithms in the Correlation of Thermal Mathematical Models of Spacecrafts ' , International Journal of Aerospace Engineering , vol. 2017 , 7683457 , pp. 1-12 . https://doi.org/10.1155/2017/7683457 | |
dc.identifier.doi | 10.1155/2017/7683457 | |
dc.identifier.issn | 1687-5966 | |
dc.identifier.other | researchoutputwizard: 11556/406 | |
dc.identifier.url | http://www.scopus.com/inward/record.url?scp=85021739915&partnerID=8YFLogxK | |
dc.language.iso | eng | |
dc.relation.ispartof | International Journal of Aerospace Engineering | |
dc.rights | info:eu-repo/semantics/openAccess | |
dc.subject.keywords | Thermal Mathematical Model | |
dc.subject.keywords | Space | |
dc.subject.keywords | Correlation | |
dc.subject.keywords | Model adjustment | |
dc.subject.keywords | Optimization | |
dc.subject.keywords | Gradient-Based solutions | |
dc.subject.keywords | Genetic algorithms | |
dc.subject.keywords | Thermal Mathematical Model | |
dc.subject.keywords | Space | |
dc.subject.keywords | Correlation | |
dc.subject.keywords | Model adjustment | |
dc.subject.keywords | Optimization | |
dc.subject.keywords | Gradient-Based solutions | |
dc.subject.keywords | Genetic algorithms | |
dc.subject.keywords | Aerospace Engineering | |
dc.title | Performance of Gradient-Based Solutions versus Genetic Algorithms in the Correlation of Thermal Mathematical Models of Spacecrafts | en |
dc.type | journal article |
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