Fault tolerant flight control system for the tilt-rotor UAV

Author:

Park Sewook,Bae Jonghee,Kim Youdan,Kim Sungwan

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Networks and Communications,Signal Processing,Control and Systems Engineering

Reference27 articles.

1. S.J. Hwang, M.K. Lee, Y.S. Kim, J.M. Kim, Prop-rotor load evalution in collision avoidance maneuver of tilt rotor unmanned aerial vehicle, in: Proceedings of the AHS Vertical Lift Aircraft Design Conference, San Francisco, CA, Jan. 2006.

2. J.H. Lee, B.M. Min, E.T. Kim, Autopilot design of tilt-rotor UAV using particles swarm optimization method, in: Proceedings of the International Conference on Control, Automation and Systems, Seoul, Korea, Oct. 2007.

3. Model following reconfigurable flight control system for the AFRI/F-16;Morse;Journal of Guidance, Control, and Dynamics,1990

4. Design of restructuable flight control systems using feedback linearization;Ochi;Journal of Guidance, Control, and Dynamics,1991

5. Reconfigurable flight control system design using direct adaptive method;Kim;Journal of Guidance, Control, and Dynamics,2003

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