DocumentCode :
583685
Title :
Collision avoidance of Smart UAV in multiple intruders
Author :
Yoo, Chang-Sun ; Cho, Am ; Park, Bum-Jin ; Kang, Young-shin ; Shim, Sang-Wook ; Lee, Il-Hyung
Author_Institution :
UAV Syst. Div., Korea Aerosp. Res. Inst., Daejeon, South Korea
fYear :
2012
fDate :
17-21 Oct. 2012
Firstpage :
443
Lastpage :
447
Abstract :
Collision avoidance of UAV is an important function required from pilots and traffic controller as it intends to fly in the airspace of manned aircraft. It is implemented into Smart UAV which the flight test for automatic take-off, conversion and mission flight was conducted successfully last year. Prior to flight test for collision avoidance, the hardware-in-the-loop simulation (HILS) test is conducted in order to verify system operation and avoidance algorithm. Intruders are simulated through virtual aircraft models on the ground and transmitted to digital flight control computer (DFCC). The detection and avoidance algorithm is implemented to the operational flight program (OFP) in DFCC. This paper gives the description for the configuration of collision avoidance system, HILS system and the result for the simulation test in the case of multiple intruders.
Keywords :
aerospace control; aircraft; autonomous aerial vehicles; collision avoidance; traffic control; HILS test; automatic take-off; collision avoidance system; digital flight control computer; hardware-in-the-loop simulation; mission flight; multiple intruders; operational flight program; pilots; smart UAV; system operation; traffic controller; virtual aircraft models; Aerospace control; Aircraft; Aircraft navigation; Atmospheric modeling; Collision avoidance; Computational modeling; Electronic mail; Digital Flight Control Computer; Hardware-In-the-Loop Simulation; Smart UAV; collision avoidance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems (ICCAS), 2012 12th International Conference on
Conference_Location :
JeJu Island
Print_ISBN :
978-1-4673-2247-8
Type :
conf
Filename :
6393481
Link To Document :
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