Article Information  
A Hybrid Flight Control for a Simulated Raptor-30 V2 Helicopter

Keywords: Hybrid Control System, PID, Fuzzy Logic, X-Plane, Helicopter Model

Mehran University Research Journal of Engineering & Technology

Volume 34 ,  Issue 2


1. Martinez, M.L., Ortega, M.G., Vivas, C., and Rubio, F.R., “Nonlinear L2 Control of a Laboratory Helicopter with Variable Speed Rotors”, Automatica, Volume 43, No.4, pp. 655-661, 2007
2. Khizer, A.N., Yaping, D.,Ali,S.A., and Xiangyang, X., “Stable Hovering Flightof Small Unmanned Helicopter using Fuzzy Control”, Journal of Mathematical Problems in Engineering, USA, September, 2014
3. Yongquan, Y., Ying, H., and Bi, Z., “A PID Neural Network Controller”, Proceedings of IJCNN, Volume 4, pp. 1933-1938, Portland, USA, 2003
4. Oliveira, V.A., Cossi, L.V., Teixeira, M., and Silva, A.M.F., “Synthesis of PID Controllers for a Class of Time Delay Systems”, Automatica, Volume 45, No.7, pp. 1778-1782, 2009
5. Albaker, B.M., and Rahim, N.A., “Flight Path PID Controller for Propeller Driven Fixed Wing Unmanned Aerial Vehicles”, International Journal of the Physical Sciences, Volume 6, No.8, pp. 1947-1964, 18 April, 2011