Minimum energy oriented global stabilizing control of the PVTOL aircraft

References

• Al-Hiddabi , S , Shen , J and McClamroch , NH . Proceedings of American Control Conference . “A study of flight maneuvers for the PVTOL aircraft model”, in , pp. 2727 – 2731 .
   Google Scholar
• Alamir , M and Marchand , n . 2003 . “Constrained sub-optimal feedback control for minimum-time stabilization of nonholonomic systems in chained form” . Journal of Optimization Theory and Applications , 118 : 229 – 244 .
   Google Scholar
• Astolfi , A . 1996 . “Discontinuous control of nonholonomic systems” . Systems & Control Letters , 27 : 37 – 45 .
   Web of Science ®Google Scholar
• Athans , M and Falb , PL . 1966 . Optimal Control , New York : McGraw Hill .
   Google Scholar
• Canudas de Witt , C and Khennouf , H . Proceedings of the Third European Control Conference . “Quasi-continuous stabilizing controllers for nonholonomic systems: design and robustness considerations”, in , pp. 2630 – 2635 .
   Google Scholar
• Di Giamberardino , P and Djemai , M . Proceedings of IEEE Conference on Decision and Control . “Multirate digital control of a PVTOL” 49 , pp. 3844 – 3849 .
   Google Scholar
• Dubins , LE . 1957 . “On curves of minimal length with a constraint on average curvature and with prescribed initial and terminal positions and tangents” . Americain Journal of Mathematics , 79 : 497 – 516 .
   Web of Science ®Google Scholar
• Fantoni , I , Zavala , A and Lozano , R . Proceedings of IEEE Conference on Decision and Control . “Global stabilization of a PVTOL aircraft with bounded thrust”, in , pp. 4462 – 4467 .
   Google Scholar
• Hably , A , Marchand , N and Alamir , M . Proceedings of IEEE Conference on Decision and Control and European Control Conference . December . “Minimum-time-oriented stabilization of extended chained form systems” , pp. 6158 – 6163 .
   Google Scholar
• Hauser , J , Sastry , S and Meyer , G . 1992 . “Nonlinear control design for slightly non-minimum phase systems: application to v/stol aircraft” . Automatica , 28 : 665 – 679 .
   Web of Science ®Google Scholar
• Hauser , J , Sastry , S and Kokotovic , P . 1992b . Nonlinear control via approximated input-output linearization: the ball and beam example . IEEE Transactions on Automatic Control , 37 : 392 – 398 .
   Web of Science ®Google Scholar
• Lin , F , Zhang , W and Brandt , RD . 1999 . “Robust hovering control of a PVTOL aircraft” . IEEE Transactions on Control Systems Technology , 7 : 343 – 351 .
   Web of Science ®Google Scholar
• Marchand , N and Hably , A . 2005 . “Global stabilization of multiple integrators with bounded controls” . Automatica , 41 : 2147 – 2152 .
   Web of Science ®Google Scholar
• Martin , P , Devasia , S and Paden , B . 1996 . “A different look at output tracking: control of a vtol aircraft” . Automatica , 32 : 101 – 107 .
   Web of Science ®Google Scholar
• Olfati-Saber , R . 2002 . “Global configuration stabilization for the VTOL aircraft with strong input coupling” . Transactions on Automatic Control , 47 : 1949 – 1952 .
   Web of Science ®Google Scholar
• Pamolino , A , Castillo , P , Fantoni , I , Lozano , R and Pégard , C . Proceedings of IEEE Conference on Decision and Control . “Control strategy using vision for the stabilization of an experimental PVTOL aircraft setup”, in , pp. 4487 – 4492 .
   Google Scholar
• Reyhanoglu , M , Cho , S , McClamroch , NH and Kolmanovsky , I . Proceedings of 37th Conference on Decision and Control . “Discontinuous feedback control a planar rigid body with an underactuated degree of freedom”, in , pp. 433 – 438 .
   Google Scholar
• Sira-Ramirez , H and Fliess , M . Proceedings of IEEE Conference on Decision and Control . “Regulation of non-minimum phase outputs in a PVTOL aircraft”, in , pp. 4222 – 4227 .
   Google Scholar
• Souéres , P , Balluchi , A and Bicchi , A . 2001 . “Optimal feedback control for route tracking with a bounded-curvature vehicle” . International Journal of Control , 74 : 1009 – 1019 .
   Web of Science ®Google Scholar
• Teel , AR . 1992 . “Global stabilization and restricted tracking for multiple integrators with bounded controls” . Systems & Control Letters , 18 : 165 – 171 .
   Web of Science ®Google Scholar
• Teel , AR , Murray , RM and Walsh , GC . 1995 . “Non-holonomic control systems: from steering to stabilization with sinusoids” . International Journal of Control , 62 : 849 – 870 .
   Web of Science ®Google Scholar
• Yang , JY , Sontag , ED and Sussmann , HJ . 1997 . “Global stabilization of linear discrete-time systems with bounded feedback” . Systems & Control Letters , 30 : 273 – 281 .
   Web of Science ®Google Scholar
• Zavala , A , Fantoni , I and Lozano , R . 2003 . “Global stabilization of a PVTOL aircraft with bounded inputs” . International Journal of Control , 76 : 1833 – 1844 .
   Web of Science ®Google Scholar
• Zhang , S and Jin , J . 1996 . Computation of Special Functions , New York : Wiley .
   Google Scholar