Journal
IFAC PAPERSONLINE
Volume 50, Issue 1, Pages 2720-2725Publisher
ELSEVIER SCIENCE BV
DOI: 10.1016/j.ifacol.2017.08.576
Keywords
Sliding-mode control; robustness; stability analysis; Lyapunov stability; quadrotors; Newton-Euler equations
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Funding
- INRIA-Lille Nord Europe
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This paper considers the problem of attitude and altitude control of quadrotors using the sliding mode control theory. The mathematical model of the quadrotor is derived using the Euler-Newton formalism with extended assumptions on disturbing aerodynamical forces (not necessary uniformly bounded). The proposed control demonstrates an enhanced robustness against such disturbances. The comparison between the classical controller and the proposed one is demonstrated analytically, through Lyapunov theory, and in simulations to validate the proposed sliding mode control algorithm. (C) 2017, IFAC (International Federation of Automatic Control) Hosting by Elsevier Ltd. All rights reserved.
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