Development of the Test Platform for Rotary Wing Unmanned Air Vehicle
Öz
In this study, a new test platform was developed for rotary wing unmanned air vehicle (UAV) with the multirotors.
This platform basically includes three different sized circles. Before the flight of UAV, all tests such as yaw,
pitch, roll, elevation, etc., are done by the proposed test platform, so the problem or crash in flight of UAV will be
prevented. The developed test platform is more superior to the existing test platforms. In this work, the detailed
developing process of test platform is presented and some pre-flight tests done by this test platform are represented
for the rotary wing UAV with six rotors.
Anahtar Kelimeler
Kaynakça
- How, J. P., Bethke, B., Frank, a., Dale, D., & Vian, J., "Real-time Indoor Autonomous Vehicle Test Environment", IEEE Control Systems, vol. 28(2), pp. 51–64, 2008.
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- Hanford, S. D., Long, L. N., & Horn, J. F., "A Small Semi-Autonomous Rotary-Wing Unmanned Air Vehicle ( UAV)", American Institute of Aeronautics and Astronautics Conference 2005, pp.1–10.
- Volkmann, O., "Multirotor 101" published in Drone 360 on the website. [Online]. Available: https://www.habanaavenue.com/2015/05/14/multirotor-101
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- Yu, Y., & Ding, X., "A Quadrotor Test Bench for Six Degree of Freedom Flight. Journal of Intelligent and Robotic Systems: Theory and Applications, vol. 68(3-4), pp. 323–338, 2012.
- Artale, V., Milazzo, C. L. R., & Riccardello, a., "Mathematical Modeling of Hexacopter". Applied Mathematical Sciences, vol. 7(97), pp. 4805–481, 2013.
- Grzonka, S., Grisetti, G., Burgard, W., A Fully Autonomous Indoor Quadrotor, IEEE Transactions On Robotics, vol. 28, pp. 90-100, 2011.
Ayrıntılar
Birincil Dil
Türkçe
Konular
-
Bölüm
Araştırma Makalesi
Yayımlanma Tarihi
16 Aralık 2016
Gönderilme Tarihi
20 Kasım 2017
Kabul Tarihi
-
Yayımlandığı Sayı
Yıl 2016 Cilt: 3 Sayı: 2