
Exploration of the basic flight mode of a two-axis aircraft
Author(s) -
Xuetao Liu
Publication year - 2019
Publication title -
iop conference series. earth and environmental science
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.179
H-Index - 26
eISSN - 1755-1307
pISSN - 1755-1315
DOI - 10.1088/1755-1315/295/3/032086
Subject(s) - aeronautics , drone , aerospace engineering , computer science , mode (computer interface) , engineering , simulation , human–computer interaction , genetics , biology
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.