DocumentCode
2258298
Title
An improved nonlinear guidance law for unmanned aerial vehicles path following
Author
Hui, Mao Yun ; Yang, Chen Qing ; Xi, Hou Zhong ; Zheng, Guo
Author_Institution
Institute of Nearspace Technology, College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, China, 410073
fYear
2015
fDate
28-30 July 2015
Firstpage
5271
Lastpage
5276
Abstract
To guarantee the UAVs path following accuracy and guarantee the ability of anti-disturbance, an improved nonlinear path following method for UAVs is proposed in the paper. Based on the nonlinear guidance logic, the virtual target on the path is confirmed and the instantaneous lateral acceleration of UAVs is calculated. What´s more, to compensate other uncertain factors in the path following process such as model uncertainty or other disturbances (wind etc), a feed-back term is added accordingly. Simulations are carried out, including the straight line and curved circle path following experiments, to verify the advantages of the proposed method.
Keywords
Acceleration; Aerospace control; Aerospace engineering; Electronic mail; Trajectory; Vehicle dynamics; Vehicles; Feedback term; Nonlinear guidance logic; Path following;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7260462
Filename
7260462
Link To Document