Global finite-time stabilization of a PVTOL aircraft by output feedback
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[1] S. Bhat,et al. Continuous finite-time stabilization of the translational and rotational double integrators , 1998, IEEE Trans. Autom. Control..
[2] A. Teel. A nonlinear small gain theorem for the analysis of control systems with saturation , 1996, IEEE Trans. Autom. Control..
[3] Dennis S. Bernstein,et al. Geometric homogeneity with applications to finite-time stability , 2005, Math. Control. Signals Syst..
[4] Yiguang Hong,et al. Finite-time stabilization and stabilizability of a class of controllable systems , 2002, Syst. Control. Lett..
[5] Chunjiang Qian,et al. Global stabilization of a class of upper‐triangular systems with unbounded or uncontrollable linearizations , 2011 .
[6] Chunjiang Qian,et al. Control of a PVTOL Aircraft using Finite-Time Output Feedback , 2009 .
[7] Hong Wang,et al. Stabilization of a PVTOL Aircraft and an Inertia Wheel Pendulum Using Saturation Technique , 2007, IEEE Transactions on Control Systems Technology.
[8] Rogelio Lozano,et al. Global stabilization of a PVTOL aircraft model with bounded inputs , 2003 .
[9] B. Paden,et al. A different look at output tracking: control of a VTOL aircraft , 1994, Proceedings of 1994 33rd IEEE Conference on Decision and Control.
[10] Jie Huang,et al. On an output feedback finite-time stabilization problem , 2001, IEEE Trans. Autom. Control..
[11] S. Shankar Sastry,et al. Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft , 1992, Autom..
[12] Rogelio Lozano,et al. Control of Nonlinear Mechanical Systems , 2001, Eur. J. Control.