期刊
JOURNAL OF INTELLIGENT & ROBOTIC SYSTEMS
卷 69, 期 1-4, 页码 161-169出版社
SPRINGER
DOI: 10.1007/s10846-012-9731-4
关键词
Multi rotor UAV; Modeling; Sliding mode; Real-time
资金
- CONACyT
In this paper, a nonlinear control augmented system for a novel eight rotor helicopter is developed, in order to achieve hover flight. Simulation results underline the good performance of the proposed control strategy. Experimental tests have been performed showing the reliability of the proposed approach.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据