Landing Control System Design for a Flying-Wing Aircraft Based on ADRC

被引：0
|
作者：
Wang, Yanxiong [1 ]
Zhu, Xiaoping [2 ]
Zhou, Zhou [1 ]
Shao, Zhuang [1 ]
机构：
[1] Northwestern Polytech Univ, Sci & Technol UAV Lab, Xian 710065, Peoples R China
[2] Northwestern Polytech Univ, UAV Res Inst, Xian 710065, Peoples R China
来源：
INTELLIGENT ROBOTICS AND APPLICATIONS, ICIRA 2014, PT I | 2014年 / 8917卷
关键词：
nonlinear control; active disturbance rejection control; control allocation; wind encounters; ground effect; flying-wing aircraft; FLIGHT CONTROL;
D O I：
暂无
中图分类号：
TP18 [人工智能理论];
学科分类号：
081104 ; 0812 ; 0835 ; 1405 ;
摘要：
In this paper, the flight simulation and control of a flying-wing aircraft in landing is presented. Significant dynamic nonlinearity and atmospheric disturbance are main problems for a flying-wing aircraft in landing phase. Therefore, a nonlinear controller with strong robustness is required. Active disturbance rejection control technique is used to design the controller which could estimate and compensate the uncertainties. A landing condition in which the wind shear encounters and ground effect before touchdown is considered, and a nonlinear longitudinal dynamic model of flying-wing aircraft in variable wind field is established. Simulations are conducted in MATLAB and the controller is shown to suppress the wind effects and ground proximity.
引用
收藏
页码：340 / 351
页数：12
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