Aerodynamic Parameter Estimation for a Morphing Unmanned Aerial Vehicle from Flight Tests

被引：3

作者：

Hui, Zhe ^{[1
,3
]}

Chen, Gang ^{[2
,3
]}

机构：

[1] Xi An Jiao Tong Univ, Sch Aerosp Engn, Xian 710049, Peoples R China

[2] Xi An Jiao Tong Univ, State Key Lab Strength & Vibrat Mech Struct, Xian 710049, Peoples R China

[3] Xidian Univ, Sch Aerosp Sci & Technol, Xian, Shaanxi, Peoples R China

来源：

JOURNAL OF AEROSPACE INFORMATION SYSTEMS | 2023年 / 20卷 / 09期

关键词：

Flight Testing; Unmanned Aerial Vehicle; Flight Control Surfaces; Flight Mechanics; Aerodynamic Characteristics; Aerodynamic Performance; System Identification; Wind Tunnel Tests; Morphing Wing; SYSTEM-IDENTIFICATION; MODEL IDENTIFICATION;

D O I：

10.2514/1.I011183

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：588 / 595

页数：8

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