Modeling and Control of Tilt-rotor Aircraft

被引：0

作者：

Lu Ke ^{[1
,2
]}

Liu Chunsheng ^{[2
]}

Wang Zhengzhong ^{[1
]}

Wang Weihong ^{[3
]}

机构：

[1] CHRDI, Sci & Technol Rotorcraft Aeromech Lab, Jingdezhen 333001, Peoples R China

[2] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Jiangsu, Peoples R China

[3] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China

来源：

PROCEEDINGS OF THE 28TH CHINESE CONTROL AND DECISION CONFERENCE (2016 CCDC) | 2016年

关键词：

tiltrotor aircraft; flight dynamics; flight control;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this paper, a flight dynamics model of a tiltrotor aircraft is developed used basic equations of motion. This model focuses on control aspect of tiltrotor and is able to show inherent tiltrotor characteristics; then a flight control system is designed used novel L-1 adaptive control theory. The XV-15 tilt rotor aircraft is taken as an example to verify this modeling method and flight control system; finally, numerical simulations are presented to show the performance and robustness of the proposed controller.

引用

页码：550 / 553

页数：4

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