[1]
|
R. H. Stone, “The T-wing Tail-Sitter Unmanned Air Vehicle: From Design Concept to Research Flight Vehicle,” Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 218, No. 6, 2004, pp. 417-433. doi:10.1243/0954410042794920
|
[2]
|
J. Carl G. Schaefer and L. J. Baskett, “GoldenEye: The Clandestine UAV,” in 2nd AIAA “Unmanned Unlimited” Systems, Technologies, and Operations, 2003, pp. 1-11.
|
[3]
|
J. Escareno, R. H. Stone, A. Sanchez and R. Lozano, “Modeling and Control Strategy for the Transition of a Convertible Tail-sitter UAV,” in European Control Conference, 2007.
|
[4]
|
O. Harkegard, “Flight Control Design Using Backstepping,” Linkoping University, 2003.
|
[5]
|
N. B. Knoebel and T. W. McLain, “Adaptive Quaternion Control of A Miniature Tailsitter UAV,” in 2008 American Control Conference, 2008, pp. 2340-2345. doi:10.1109/ACC.2008.4586841
|
[6]
|
A. A. Mian, M. I. Ahmad and D. Wang, “Backstepping based Nonlinear Flight Control Strategy for 6 DOF Aerial Robot,” in 2008 International Conference on Smart Manufacturing Application, 2008, pp. 146-151. doi:10.1109/ICSMA.2008.4505630
|
[7]
|
F. M. Subolic, “Agile Flight Control Techniques for a Fixed-Wing Aircraft,” Massachusetts Institute of Technology, 2009.
|
[8]
|
J. H. Yang and W. C. Hsu, “Adaptive Backstepping Control for Electrically Driven Unmanned Helicopter,” Control Engineering Practice, Vol. 17, No. 8, 2009, pp. 903-913. doi:10.1016/j.conengprac.2009.02.012
|
[9]
|
W. S. Lohmiller, “Contraction Analysis of Nonlinear Systems,” Massachusetts Institute of Technology, 1999.
|
[10]
|
W. Lohmiller and J. J. E. Slotine, “On Contraction Analysis for Non-linear Systems,” Automatica, Vol. 34, No. 6, 1998, pp. 683-696. doi:10.1016/S0005-1098(98)00019-3
|
[11]
|
W. Lohmiller and J. J. E. Slotine, “Control System Design for Mechanical Systems Using Contraction Theory,” IEEE Transactions on Automatic Control, Vol. 45, No. 5, 2000, pp. 984-989. doi:10.1109/9.855568
|
[12]
|
J. Jouffroy and J. J. E. Slotine, “Methodological Remarks on Contraction Theory,” 2004 43rd IEEE Conference on Decision and Control (CDC) (IEEE Cat. No.04CH37601) , Vol. 3, 2004, pp. 2537-2543.
|
[13]
|
J. Jouffryo, “Integrator Backstepping Using Contraction Theory: A Brief Methodological Note,” 2002, p. 238.
|
[14]
|
B. B. Sharma and I. N. Kar, “Contraction Theory-based Recursive Design of Stabilising Controller for A Class of Non-linear Systems,” IET Control Theory & Applications, Vol. 4, No. 6, 2010, p. 1005. doi:10.1049/iet-cta.2009.0060
|
[15]
|
M. Zamani and P. Ta-buada, “Towards Backstepping Design for Incremental Stability,” 49th IEEE Conference on Decision and Control (CDC) , 2010, pp. 2426-2431. doi:10.1109/CDC.2010.5717210
|
[16]
|
B. L. Stevens and F. L. Lewis, “Aircraft Control and Simulation,” John Wiley and Sons, 2003, p. 664.
|