DocumentCode :
1526348
Title :
Vision-Only Automatic Flight Control for Small UAVs
Author :
Chiu, Chung-Cheng ; Lo, Ching-Tung
Author_Institution :
Dept. of Electr. & Electron. Eng., Chung Cheng Inst. of Technol.-Nat. Defense Univ., Taoyuan, Taiwan
Volume :
60
Issue :
6
fYear :
2011
fDate :
7/1/2011 12:00:00 AM
Firstpage :
2425
Lastpage :
2437
Abstract :
In this paper, a vision-based flight control system that uses a skyline-detection algorithm is developed for application to small unmanned aerial vehicles. The skyline-detection algorithm can detect straight or uneven skylines. The system integrates a remote controller, a remotely controlled airplane, a camera, a wireless transmitter/receiver, a ground control computer, and the proposed skyline-detection algorithm to achieve automatic control of flight stability. Static and dynamic tests are conducted to validate the system. In the static tests, the average accuracy rate for skyline detection is 98.62% based on five test videos. In the dynamic tests, straight and circular flights are used to verify lateral and longitudinal stability for the proposed flight control system. The experimental results demonstrate the performance and robustness of the algorithm and the feasibility and potential of a low-cost vision-only flight control system.
Keywords :
aircraft control; aircraft testing; mobile robots; radio receivers; radio transmitters; remotely operated vehicles; robot vision; stability; dynamic tests; flight stability; ground control computer; low-cost vision-only automatic flight control system; remotely controlled airplane; skyline-detection algorithm; small UAV; static tests; unmanned aerial vehicles; wireless receiver; wireless transmitter; Aerospace control; Aircraft; Cameras; Image color analysis; Image edge detection; Pixel; Videos; Automated vehicles; skyline detection; vision control;
fLanguage :
English
Journal_Title :
Vehicular Technology, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9545
Type :
jour
DOI :
10.1109/TVT.2011.2157545
Filename :
5773513
Link To Document :
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