DocumentCode :
1170353
Title :
Implementation of collision avoidance system using TCAS II to UAVs
Author :
Lee, Hyeon-Cheol
Author_Institution :
Korea Aerosp. Res. Inst., Daejeon
Volume :
21
Issue :
7
fYear :
2006
fDate :
7/1/2006 12:00:00 AM
Firstpage :
8
Lastpage :
13
Abstract :
There will come the day that UAVs can fly into the airspace of manned aircraft in the near future because of the increasing number of operational UAVs, together with technologies development. Since pilots of UAVs are on the ground, the equipment for sensing and avoiding obstacles in front is indispensable. In this paper, the TCAS II, a collision avoidance device for manned aircraft, is implemented to UAVs and investigated for the interfaces of a flight control computer. It turns out that the onboard directional antenna of TCAS II does not provide precise direction information, and the TCAS II is not assumed to be installed alone, but used as supplement with other device which tells precise direction
Keywords :
aircraft computers; aircraft control; aircraft instrumentation; collision avoidance; remotely operated vehicles; TCAS II; UAV; collision avoidance; directional antenna; flight control computer; manned aircraft; Aerospace control; Aircraft manufacture; Collision avoidance; Computer interfaces; Directional antennas; Ground support; Military aircraft; Satellites; Sensor systems; Unmanned aerial vehicles;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/MAES.2006.1684262
Filename :
1684262
Link To Document :
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