Mason P, Broucke M, Piccoli B. Time optimal swing-up of the planar pendulum. IEEE Transactions on Automatic Control, 2008, 53(8): 1876-1886
[2]
Maravall D, Zhou C J, Alonso J. Hybrid fuzzy control of the inverted pendulum via vertical forces. International Journal of Intelligent Systems, 2005, 20(2): 195-211
[3]
Hauser J, Sastry S, Meyer G. Nonlinear control design for slightly non-minimum phase systems: application to V/STOL aircraft. Automatica, 1992, 28(4): 665-679
[4]
Ailon A. Simple tracking controllers for autonomous VTOL aircraft with bounded inputs. IEEE Transactions on Automatic Control, 2010, 55(3): 737-743
[5]
Consolini L, Tosques M. On the VTOL exact tracking with bounded internal dynamics via a poincaré map approach. IEEE Transactions on Automatic Control, 2007, 52(9): 1757-1762
[6]
？str？m K J, Furuta K. Swinging up a pendulum by energy control. Automatica, 2000, 36(2): 287-295
[7]
Srinivasan B, Huguenin P, Bonvin D. Global stabilization of an inverted pendulum-control strategy and experimental verification. Automatica, 2009, 45(1): 265-269
[8]
Maravall D. Control and stabilization of the inverted pendulum via vertical forces. Robotic Welding, Intelligence and Automation, Lecture Notes in Control and Information Sciences. Berlin: Springer-Verlag, 2004, 299: 190-211
[9]
Olfati-Saber R. Global configuration stabilization for the VTOL aircraft with strong input coupling. IEEE Transactions on Automatic Control, 2002, 47(11): 1949-1952
[10]
Do K D, Jiang Z P, Pan J. On global tracking control of a VTOL aircraft without velocity measurements. IEEE Transactions on Automatic Control, 2003, 48(12): 2212-2217
[11]
Wang J J. Simulation studies of inverted pendulum based on PID controllers. Simulation Modelling Practice and Theory, 2011, 19(1): 440-449
