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
收藏
页码：550 / 553
页数：4
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