DocumentCode :
1795436
Title :
Mission-oriented control scheme for autonomous/semi-autonomous UCAV
Author :
Xieyu Xu ; Lingyu Yang ; Xiao Hu ; Jing Zhang
Author_Institution :
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
2734
Lastpage :
2739
Abstract :
This paper discusses the scheme and design method for UCAV autonomous/semi-autonomous control system. According to the investigation of the traditional tactical flight maneuvers and the existing air combat simulators, a mission-oriented control scheme is proposed to fulfill the autonomous/semi-autonomous requirements. A library including 9 maneuvers is designed by which complex tasks could be formed. And base on the flight mechanics, a control structure of line motion-angular motion is proposed to simplify the implementation of flight maneuvers. Finally, the proposed method is validated through simulations of a nonlinear six degrees of freedom UAV model.
Keywords :
autonomous aerial vehicles; control system synthesis; military aircraft; mobile robots; motion control; UCAV autonomous control system; UCAV semiautonomous control system; air combat simulators; angular motion control structure; flight mechanics; line motion control structure; mission-oriented control scheme; nonlinear six degrees of freedom UAV model; tactical flight maneuvers; uninhabited combat aerial vehicles; Acceleration; Aerospace control; Aircraft; Lead; Libraries; Trajectory; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007598
Filename :
7007598
Link To Document :
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