Aerodynamic characteristic analysis and layout optimization design for compound UAVs by using hybrid Fuzzy-PSO algorithm

被引：2

作者：

Chen, Yan-li ^{[1
]}

Qin, Jing-chun ^{[1
]}

Shang, Yi-zhuo ^{[1
]}

Xu, Shi-kun ^{[1
]}

Li, Ji-cai ^{[1
]}

Zhao, Nan ^{[1
]}

Wu, Xiao-dong ^{[1
]}

Yu, Xian-li ^{[2
]}

机构：

[1] Jilin Univ, Sch Mech & Aerosp Engn, Changchun 130025, Jilin, Peoples R China

[2] Jilin Univ, Coll Geoexplorat Sci & Technol, Changchun 130026, Jilin, Peoples R China

来源：

JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING | 2019年 / 41卷 / 01期

基金：

中国博士后科学基金; 中国国家自然科学基金;

关键词：

Compound UAVs; Aerodynamic characteristics; Configuration design; Global optimization; Hybrid Fuzzy-PSO algorithm; KRIGING-MODEL;

D O I：

10.1007/s40430-018-1547-0

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

In order to further improve the performance of compound UAVs at high and low speed with heavy loading, a type of compound coaxial UAV with fixed wings and tail ducted-rotor thrusters was proposed to meet technology requirement. The lift and thrust aerodynamic characteristics were analyzed to get some relative characteristic and the aerodynamic coupling relationships between the fixed wings and tail propulsion system. And an optimization method based on hybrid Fuzzy-PSO (HFPSO) algorithm was proposed to obtain the optimal configuration plan that can reach the best aerodynamic performance without considering the coaxial architecture. The optimal configuration plan was finally obtained by applying the HFPSO method which also proves the method is effective and reasonable through comparison.

引用

页数：15

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