On Safe Landing Control Technology of Unmanned Helicopter

被引：0
|
作者：
Wang Lu [1 ]
Yao Weili [1 ]
Zhang Meng [1 ]
Huang Yimin [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 211100, Jiangsu, Peoples R China
来源：
2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2016年
关键词：
UAH; landing; touchdown; rotor speed; collective;
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 the process of unmanned helicopter landing, when gears are touching down, rotation speed of main rotor and collective will both stay at high level, which threatens landing safety severely. This paper proposes a control design aimed at the situation, and then make a proof and simulation.
引用
收藏
页码：1599 / 1604
页数：6
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