Landing Control Scheme of Vertical Take-off and Landing Fixed-wing UAV

被引：0
|
作者：
Chang, Tianxing [1 ]
Guo, Zhiming [1 ]
Zhang, Jiawei [1 ]
Wu, Liaoni [1 ]
机构：
[1] Xiamen Univ, Sch Aerosp Engn, Xiamen 361102, Peoples R China
来源：
PROCEEDINGS OF 2018 IEEE 3RD ADVANCED INFORMATION TECHNOLOGY, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (IAEAC 2018) | 2018年
关键词：
vertical take-off and landing; fixed-wing UAV; landing Control;
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：
As a new type of aircraft, vertical takeoff and landing UAV has attracted wide attention in the industry. However, it still lacks relevant research about control strategies and solutions to extreme environments. This paper designs and validates two schemes for landing modes in two special environments, including landing in high altitude and mountainous and mobile landing on the ship. First, the design of the control law is carried out step by step. Then we have plenty of flight tests and analyze lots of data. We change the control parameters to achieve the desired results. The research indicates that the two schemes are feasible in engineering practice and can provide technical references.
引用
收藏
页码：1984 / 1988
页数：5
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