Nonlinear Constrained Optimization Method for Dynamic Conversion Corridor of Tilt-Rotor Aircraft

被引：2

作者：

Song, Wei ^{[1
]}

Sun, Liguo ^{[2
]}

Wang, Qi ^{[3
]}

机构：

[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China

[2] Nanchang Hangkong Univ, Sch Aeronaut Sci & Engn, Nanchang 330063, Peoples R China

[3] Nanchang Hangkong Univ, Sch Aircraft Engn, Nanchang 330063, Peoples R China

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2024年 / 47卷 / 12期

关键词：

Optimization Algorithm; Tilt Rotor Aircraft; Aircraft Components and Structure; Aerodynamic Performance; Tail Sitter; Drag Coefficient; Dynamic Modelling; Unmanned Aerial Vehicle; Aircraft Flight Control System; Helicopters;

D O I：

10.2514/1.G007721

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：2661 / 2666

页数：6

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