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 :
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