Modeling and Control for Morphing Unmanned Aircraft Vehicle

被引：0

作者：

Li, Mengtao ^{[1
]}

Guo, Lei ^{[2
]}

Wu, Kejian ^{[3
]}

机构：

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

[2] Beihang Univ, Sci & Technol Aircraft Control Lab, Beijing 100191, Peoples R China

[3] Beihang Univ, Sch Instrumentat Sci & Optoelect Engn, Beijing 100191, Peoples R China

来源：

2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2016年

基金：

中国国家自然科学基金;

关键词：

morphing unmanned aircraft vehicle; 6DOF; modeling; nonlinear dynamic inversion method;

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：

there has been wide interest in the research of Mars exploration. Morphing unmanned aircraft vehicle (MUAV) is one of most promising vehicles to execute special tasks in Mars exploration missions for its better aerodynamic characteristics compared with the conventional fixed wing vehicle. Modeling and control for MUAV are difficult problems. In this paper, firstly, the nonlinear six-degree-of-freedom (6DOF) dynamic model for MUAV is established, considering the asymmetry of the rotating wing. Secondly, control system is presented for the morphing aircraft based nonlinear dynamic inversion method. Finally, real-time simulation results are given to illustrate the control scheme can meet the requirements of attitude control.

引用

页码：1226 / 1231

页数：6

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