Multi-objective aerodynamic shape design optimization of canard-controlled missiles for reducing induced roll

Canard-controlled missiles are popular due to their compact size and high maneuverability. However, it is well known that these missiles suffer from adverse roll properties caused by tail-fin-induced roll during canard deflection in roll maneuvers. While auxiliary systems like a free-spinning tail s...

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Veröffentlicht in:	Optimization and engineering Jg. 25; H. 2; S. 841 - 869
Hauptverfasser:	Yoo, Seungmin, Jeong, Shinkyu, Jung, Jongho, You, Kangkuk
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York Springer US 01.06.2024
Schlagworte:	Control Engineering Environmental Management Financial Engineering Mathematics Mathematics and Statistics Operations Research/Decision Theory Optimization Research Article Systems Theory Canard-controlled missile Multi-objective optimization Aerodynamic shape design Computational fluid dynamics Data mining
ISSN:	1389-4420, 1573-2924
Online-Zugang:	Volltext
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