北京理工大学珠海学院 2020届本科生毕业设计 (论文)
II
Design of automatic landing control law for fixed wing UAV
ABSTRACT
Now the development of UAV is quite rapid, many countries in the world are developing a
variety of purposes of the UAV, the performance of the UAV is constantly put forward new
requirements. Military and civil fields can often see the figure of UAV, compared with
man-machine has many advantages, can be flexible and excellent to complete the task, has been
favored by v
自动着陆控制律-1812字.pdf