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
ARBAB NIGHAT KHIZER , AMIR MAHMOOD SOOMRO , SYED AMJAD ALI ,
References
1. |
Martinez, M.L., Ortega, M.G., Vivas, C., and Rubio, F.R., “Nonlinear L2 Control of a Laboratory Helicopter with Variable Speed Rotorsâ€, 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 Controlâ€, Journal of Mathematical Problems in Engineering, USA, September, 2014 |
3. |
Yongquan, Y., Ying, H., and Bi, Z., “A PID Neural Network Controllerâ€, 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 Systemsâ€, 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 Vehiclesâ€, International Journal of the Physical Sciences, Volume 6, No.8, pp. 1947-1964, 18 April, 2011 |
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