Safe Control for Spiral Recovery of Unmanned Aerial Vehicle

被引：0
作者：
Ru, Chang-Jian [1 ]
Wei, Rui-Xuan [1 ]
机构：
[1] Air Force Engn Univ, Xian 710038, Peoples R China
来源：
ABSTRACT AND APPLIED ANALYSIS | 2014年
基金：
美国国家科学基金会;
关键词：
SLIDING-MODE CONTROL; FLIGHT CONTROL; SYSTEMS;
D O I：
10.1155/2014/983624
中图分类号：
O29 [应用数学];
学科分类号：
070104 ;
摘要：
With unmanned aerial vehicles (UAVs) widely used in both military and civilian fields, many events affecting their safe flying have emerged. That UAV's entering into the spiral is such a typical safety issue. To solve this safety problem, a novel recovery control approach is proposed. First, the factors of spiral are analyzed. Then, based on control scheduling of state variables and nonlinear dynamic inversion control laws, the spiral recovery controller is designed to accomplish guidance and control of spiral recovery. Finally, the simulation results have illustrated that the proposed control method can ensure the UAV autonomous recovery from spiral effectively.
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收藏
页数：10
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