Control System Designed for a Four Rotors Unmanned Aerial Vehicle

Abstract:

In order to achieve the autonomous flight control of the quadrotor, an autonomous flight control hardware platform was set up, with a self-assembly aircraft as the body frame. The control system was designed according to the principle of quadrotor. It includes the hardware and code. A flight control model for the four rotor aircraft was established, so as to analyze and optimize the performance. Flight test was down. And the results showed that the quadrotor was able to flight stably and be well controlled.

• Periodical: Applied Mechanics and Materials (Volumes 716-717)
• Pages: 1527-1530
• DOI: https://doi.org/10.4028/www.scientific.net/AMM.716-717.1527
• Online since: December 2014
• Authors: Wei Ming He*, Guo Jing He, Jian Qi Zhang
• Keywords: Algorithm, Control System, Four Rotor Aircraft

References

[1] S. Bouabdallahs, A. Noth and R. Siegwart: IEEE Trans-actions on Robotics and Automation, Vol. 43. (2004), p.83.

[2] L. Gin in: Principles of Helicopter Aerodynamics［M］ New York: Cambridge University Press, (2000).

[3] M. A and D. Wang: IEEE AQTR, Vol. 26. (2008), p.616.

[4] L.D. Minh: IEEE Trans. Circuits Syst, Vol. 33. (2010), p.83.

[5] C. Wang: Journal of Jilin University: Information Science Edition, Vol. 29. (2008), p.464.

[6] Y. Hou, L. Lu, S. Gao and Y. Liu: Mechanical science and technology for aerospace engineering , Vol. 31. (2012), p.359.

[7] J. Peng: School of Electronical Engineering and Automation, Vol. 42(2003), p.754.

[8] X. Li and Y. Liu: Journal of Jilin University, Vol. 29. (2011), p.70.