[1] J. M. Maciejowski, “Multivariable Feedback Design,” Addison-Wesley Publishing Company, Boston, 1989.
[2] M. Gafven, “Modelling of rhe ETH Helicoprer Laboratory Process,” Department of Automatic Control, Lund Institute of Technology, Lund, 2001.
[3] C. Barbu, R. Reginatto, A. R. Teel and L. Zaccarian, “Anti-Windup Design for Manual Flight Control,” Proceedings of American Control Conference, San Diego, 1999, pp.3186-3190,.
[4] M. Pachter and R. B. Miller, “Manual Flight Control with Saturating Actuators,” IEEE Control Systems, 1998.
[5] M. Sacki, J. Imura and Y. Wada, “Flight Control Design of Twin Rotor Helicopter Model by 2 Step Exact Linearization,” Proceedings of IEEE International Conference on Control Applications, Vol. 1, 1999, pp. 146-151.
[6] G. Mustafa and N. Iqbal, “Control Design for a Twin Rotor Helicopter Model via Exact State Feedback,” INMIC Proceedings of the 8th International Multitopic Conference, Lahore, 24-26 December 2004, pp. 706-711.
[7] F. Allg¨ower and A. Zhen, Eds., “Nonlinear Model Predictive Control,” Progress in Systems and Control Theory, Vol. 26, 2000. doi:10.1007/978-3-0348-8407-5
[8] N. Wada and M. Saeki, “An LMI Based Scheduling Algorithm for Constrained Stabilization Problems,” Systems & Control Letters, Vol. 57, No. 3, 2008, pp. 255-261. doi:10.1016/j.sysconle.2007.09.006
[9] N. Wada and M. Saeki, “A Scheduling Algorithm for Constrained Control Systems: An Approach Based on a Parameter Dependent Lyapunov Function,” Proceedings of American Control Conference, New Orleans, 2007, pp. 5200-5205.
[10] T. Hu and Z. Lin, “Control Systems with Actuator Saturation: Analysis and Design,” Springer, Berlin, 2001. doi:10.1007/978-1-4612-0205-9
[11] N. Wada and M. Saeki, “Tracking Control with Saturating Actuators: A Method Based on State-Dependent GainScheduling and ReferenceManagement,” Proceedings of 17th IFAC World Congress, Seoul, 2008