1. A. T. Kutay, et al., “Experimental results on adaptive output feedback control using a laboratory model helicopter,” IEEE Transactions on Control Systems Technology, vol. 13, no. 2, pp. 196–202, March 2005. [click]
2. B. Zheng and Y. Zhong, “Robust attitude regulation of a 3-DOF helicopter benchmark-theory and experiments,” IEEE Transactions on Industrial Electronics, vol. 58, no. 2, pp. 660–670, March 2011. [click]
3. M. Ishitobi, M. Nishi, and M. Miyachi, “Nonlinear model following control with parameter identification for a 3-DOF model helicopter,” Proc. of IEEE/ASME International Conf. Advanced Intelligent Mechatronics, pp. 1–6, 2007. [click]
4. I. Postlethwaite, I. Prempain, E. Turkoglu, C. M. Tuner, K. Ekkis, and A. W. Gubbels, “Design and flight testing of various h-infinity controllers for the Bell 205 helicopter,” Control Engineering Practice, vol. 13, no. 3, pp. 383–398, March 2005. [click]
5. H. Sira-Ramirez, M. Zribi, and S. Ahmad, “Dynamical sliding mode control approach for vertical flight regulation in helicopters,” IEEE Proceeding Control Theory and Application, pp. 19–24, 1994. [click]