Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
710465 | IFAC-PapersOnLine | 2016 | 6 Pages |
Abstract
In this paper, an autopilot for attitude tracking is designed using disturbance compensation techniques. The proposed controller uses backstepping design procedure and combines the feedback linearization technique with high-order sliding-modes based identification for fault tolerant control. System faults and external disturbances are compensated by a differentiable term generated by means of the robust exact high-order sliding-modes differentiator. The control signal generated for the controller does not require filtration. Simulations illustrate the performance of the proposed controller in the rigid body model of an F-16 aircraft.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
J. Dávila, J. Cieslak, D. Henry,