DocumentCode :
2992524
Title :
The Guidance and Control of Small Net-recovery UAV
Author :
Chen, Jiatong ; Wang, Yong
Author_Institution :
Res. Inst. of Unmanned Aerial Vehicle, Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2011
fDate :
3-4 Dec. 2011
Firstpage :
1566
Lastpage :
1570
Abstract :
The guidance and control of net-recovery UAV based on airborne electro-optical vision guidance are proposed, because of disadvantages of the low precision, security and the dependence of data link in general recovery approaches. Optical visual guidance system is installed on the UAV, which can provide line of sight angle information for the net-recovery flight. In order to make UAV recover precisely along the expected glide path, guidance and control with line-of-sight angle of the net-recovery UAV was raised, designing strong anti-jamming control structure. Direct force control was adopted in the longitudinal control of the net-recovery UAV, increasing the agility of control. Dynamic parameter adjustment of control law based on the distance between the UAV and net was designed, which guaranteed the stability of whole recovery process. The aircraft recovery simulation of verified the guidance plan and the precision of small net-recovery UAV control.
Keywords :
aircraft control; computer vision; remotely operated vehicles; stability; airborne electro-optical vision guidance; aircraft recovery simulation; anti-jamming control structure; control law; direct force control; dynamic parameter adjustment; guidance plan; longitudinal control; optical visual guidance system; small net-recovery UAV; stability; Aerospace control; Atmospheric modeling; Azimuth; Control systems; Electrooptical waveguides; Elevators; Process control; PID; airborne electro-optical vision guidance; direct force control; dynamic parameter adjustment; net-recovery;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Intelligence and Security (CIS), 2011 Seventh International Conference on
Conference_Location :
Hainan
Print_ISBN :
978-1-4577-2008-6
Type :
conf
DOI :
10.1109/CIS.2011.351
Filename :
6128392
Link To Document :
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