Сибирский федеральный университет

Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций

Конференция: International Conference on Information Technologies, InfoTech 2018; Varna; Varna

Год издания: 2018

Идентификатор DOI: 10.1109/InfoTech.2018.8510715

Ключевые слова: differential evolution, global trajectory optimization, spacecraft trajectory optimization

Аннотация: The paper describes application of differential evolution with modified mutation strategy to the global trajectory optimization problems. The problems are provided by the European Space Agency and represent trajectories of several well-known spacecraft, namely, Cassini, Rosetta and Messenger. Using archive based differential evolution, global best solutions were found for these problems, and the best known solution was found for the Cassini mission.

Журнал: 2018 International Conference on Information Technologies, InfoTech 2018 - Proceedings

Номера страниц: 8510715

Издатель: Institute of Electrical and Electronics Engineers Inc.

• Stanovov V. (Reshetnev Siberian State University of Science and Technology)
• Akhmedova S. (Reshetnev Siberian State University of Science and Technology)
• Semenkin E. (Reshetnev Siberian State University of Science and Technology)

• Ядро РИНЦ (eLIBRARY.RU)