期刊名称：IOP Conference Series: Earth and Environmental Science
印刷版ISSN：1755-1307
电子版ISSN：1755-1315
出版年度：2019
卷号：295
期号：3
页码：1-7
DOI：10.1088/1755-1315/295/3/032086
出版社：IOP Publishing
摘要：In recent years, drones have been widely used in military and civilian applications. Among them, multi-rotor UAVs have functions such as taking off and landing vertically, hovering and flighting in high speed. It is simple to operate, safe, reliable and highly serviceable. It has received great attention from people and has become a research hotspot in recent years. However, it has obvious defects in endurance performance and load capacity, and the two-axis aircraft is one of the methods to solve the problem. Therefore, this paper explores the structural form of the two-axis aircraft and the flight principle of the basic flight mode.
