Hyper heuristic approach for design and optimization of satellite launch vehicle

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作者：
Department of Spacecraft Technology, School of Astronautics, Beihang University, Beijing 100191, China [1 ]
不详 [2 ]
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来源：
Chin J Aeronaut | / 2卷 / 150-163期
关键词：
Compilation and indexing terms; Copyright 2025 Elsevier Inc;
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摘要：
Design aids - Iterative methods - Launch vehicles - Product design - Heuristic methods - Vehicle performance - Conceptual design - Satellites
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