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IJSTR >> Volume 3- Issue 6, June 2014 Edition



International Journal of Scientific & Technology Research  
International Journal of Scientific & Technology Research

Website: http://www.ijstr.org

ISSN 2277-8616



Development Of Robust Flight Control Design For Unmanned Aerial Helicopter

[Full Text]

 

AUTHOR(S)

May Zin Tun, Zaw Min Naing, Hla Myo Tun

 

KEYWORDS

Keywords: UAV, Flight Control, Robust Control, Helicopter, MATLAB

 

ABSTRACT

Abstract: A complete flight control scheme with detailed design methodology is proposed for an indoor miniature coaxial helicopter with fixed collective pitch. To avoid system complexity and the problem of minimum phase control, the helicopter dynamic model is decomposed into two cascaded subsystems: an inner one for attitude and heading control and the outer one for trajectory control. H-infinity control technique and robust and perfect tracking method are used to respectively design the inner- and outer-loop controllers. By using the so-called asymptotic time-scale and eigenstructure assignment approach, the design process becomes very systematic and effective. The rotor simulation are also mentioned to improve the stability of UAH. The performance of the autonomous flight control system has been successfully validated in simulation flight tests.

 

REFERENCES

[1] K. Nonami, F. Kendoul, S. Suzuki, W. Wang, and D. Nakazawa, Autonomous Flying Robots: Unmanned Aerial Vehicles and Micro Aerial Vehicles, Springer, 2010.

[2] H. Lim and S. Machida,“Mechanism and Control of Coaxial Double Contra-Rotation Flying Robot,” in Proceedings of International Conference on Control, Automation and System, Gyeonggi-do, Korea, October 27-30, 2010, pp. 1109-1114.

[3] P. Fankhauser, S. Bouabdallah, S. Leutenegger, and R. Siegwart, “Modeling and Decoupling Control of the CoaX Micro Helicopter,” in Proceedings of IEEE/RSJ International Conference on Intelligent Robots and Systems, San Francisco, USA, September 25-30, 2011, pp.2223-2228.

[4] D. Schafroth, C. Bermes, S. Bouabdallah, and R.Siegwart, “Modeling, System Identification and Robust Control of a Coaxial Micro Helicopter,” Control Engineering Practice, Vol. 18, pp. 700-711, 2010.

[5] B. Vidolov, J. De Miras, and S. Bonnet, “A Two-Rule-Based Fuzzy Logic Controller for Contrarotating Coaxial Rotors UAV,” in Proceedings of IEEE International Conference on Fuzzy Systems, Vancouver, Canada, July 16-21, 2006, pp. 1563-1569.

[6] S. P. Soundararaj, A. K. Sujeeth, and A. Saxena, “Autonomous Indoor Helicopter Flight using a Single Onboard Camera,” in Proceedings of IEEE/RSJ International Conference on intellegent Robtos and Systems, St. Louis, USA, October 11-15, 2009, pp. 5307-5134.

[7] S. Wu, Z. Zheng, and K. Cai, “Indoor Autonomous Hovering Control for a Small Unmanned Coaxial Helicopter,” in Proceedings of the 8th IEEE International Conference on Control and Automation, Xiamen, China, June 9-11, 2010, pp. 267-272.

[8] H. Wang, D. Wang, X. Niu, and H. Duan, “Modeling and Hovering Control of a Novel Unmanned Coaxial Rotor/Ducted-Fan Helicopter,” in Porceedings of IEEE International Conference on Automation and Logistics, Jinan, China, August 18-21, 2007, pp.1768-1773.

[9] B. Arama, S. Barissi, and N. Houshangi, “Control of an Unmanned Coaxial helicopter Using Hybrid Fuzzy-PID Controllers,” in Proceedings of the 24th Canadian Conference on Electrical and Computer Engineering, Niagara Falls, Canada, May 8-11, 2011, pp. 1064-1068.

[10] F. Wang, S. K. Phang, J. Cui, B. M. Chen, T. H. and Lee, “Nonlinear Modeling of a Miniature Fixed-Pitch Coaxial UAV,” accepted by the 2012 American Control Conference.

[11] B. M. Chen, Robust and H∞ Control, London: Springer-Verlag, 2000.