Fast convergent observer design for output feedback stabilisation of a planar vertical takeoff and landing aircraft

IET Control Theory and Applications

Volumn 4, Issue 4, 2010, Pages 690-700

  Frye, M T ^a   Ding, S ^b   Qian, C ^c   Li, S ^b  

^a UNIVERSITY OF THE INCARNATE WORD   (United States)

^b SOUTHEAST UNIVERSITY   (China)

^c University of Texas at San Antonio   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ESTIMATED STATE; FINITE TIME; NON-LINEAR MODEL; OBSERVER DESIGN; OUTPUT FEEDBACK; OUTPUT FEEDBACK CONTROLLER; PLANAR VERTICAL TAKE-OFF AND LANDING AIRCRAFTS; STABILISATION; STABILISER; UNKNOWN STATE; VERTICAL TAKE-OFF AND LANDINGS;

FEEDBACK; LANDING; NONLINEAR FEEDBACK; TAKEOFF; UNMANNED VEHICLES; VTOL/STOL AIRCRAFT;

STATE FEEDBACK;

EID: 77955225869     PISSN: 17518644     EISSN: 17518652     Source Type: Journal    
DOI: 10.1049/iet-cta.2009.0158     Document Type: Article

References (15)

1. Hauser, J., Sastry, S., and Meyer, G.: ' Nonlinear control design for slightly nonminimum phase systems: application to V/STOL aircraft ', Automatica, 1992, 28, p. 665-679
2. Martin, P., Devasia, S., and Paden, B.: ' A different look at output tracking: control of a vtol aircraft ', Automatica, 1996, 32, p. 101-107
3. Ye, H.W., Wang, H., and Wang, H.B.: ' Stabilization of a PVTOL aircraft and an inertia wheel pendulum using saturation technique ', IEEE Trans. Autom. Control, 2007, 15, p. 1143-1150
4. Wang, X.H., Yang, G., and Xu, W.L.: ' Output tracking for nonlinear non-minimum phase systems and application to PVTOL aircraft ', Int. J. Syst. Sci., 2008, 39, p. 29-42
5. Teel, A.R.: ' A nonlinear small gain theorem for the analysis of control systems with saturation ', IEEE Trans. Autom. Control, 1996, 41, p. 1256-1270
6. Fantoni, I., and Lozano, R.: ' Control of nonlinear mechanical systems ', Eur. J. Control, 2001, 7, p. 328-348
7. Chemori, A., and Marchand, N.: ' A prediction-based nonlinear controller for stabilization of a non-minimum phase PVTOL aircraft ', Int. J. Robust Nonlinear Control, 2008, 18, p. 876-889
8. Zavala, A., Fantoni, A.I., and Lozano, R.: ' Global stabilization of a pvtol aircraft with bounded inputs ', Int. J. Control, 2003, 76, p. 1833-1844
9. Bhat, S.P., and Bernstein, D.S.: ' Continuous finite-time stabilization of the translational and rotational double integrators ', IEEE Trans. Autom. Control, 1998, 43, p.678-682
10. Hong, Y.G., Huang, J., and Xu, Y.S.: ' On an output feedback finite-time stabilization problem ', IEEE Trans. Autom. Control, 2001, 46, p. 305-309
11. Hong, Y.G.: ' Finite-time stabilization and stabilizability of a class of controllable systems ', Syst. Control Lett., 2002, 46, p. 231-236
12. Frye, M.T., Ding, S.H., Qian, C., and Colgren, R.: ' Control of a PVTOL aircraft using finite-time output feedback ', 2009 AIAA GNC Conf., AIAA-2009-6074
13. Hermes, H.: ' Homogeneous coordinates and continuous asymptotically stabilizing feedback controls ', Diff. Equ. Stab. Control, 1991, 109, p. 249-260
14. Bhat, S.P., and Bernstein, D.S.: ' Geometric homogeneity with applications to finite-time stability ', Math. Control, Signals Syst., 2005, 17, p. 101-127
15. Khalil, H.K.: ' Nonlinear systems ', 3rd (Prentice-Hall, 2002)