• Corpus ID: 17656743

Sliding Mode Control Based on Backstepping Approach for an UAV Type-Quadrotor

@article{Bouadi2007SlidingMC,
  title={Sliding Mode Control Based on Backstepping Approach for an UAV Type-Quadrotor},
  author={Hakim Bouadi and Mouloud Bouchoucha and Mohamed Tadjine},
  journal={World Academy of Science, Engineering and Technology, International Journal of Mechanical, Aerospace, Industrial, Mechatronic and Manufacturing Engineering},
  year={2007},
  volume={1},
  pages={39-44}
}
  • H. Bouadi, M. Bouchoucha, M. Tadjine
  • Published 27 February 2007
  • Engineering
  • World Academy of Science, Engineering and Technology, International Journal of Mechanical, Aerospace, Industrial, Mechatronic and Manufacturing Engineering
In this paper; we are interested principally in dynamic modelling of quadrotor while taking into account the high-order nonholonomic constraints in order to develop a new control scheme as well as the various physical phenomena, which can influence the dynamics of a flying structure. These permit us to introduce a new state-space representation. After, the use of Backstepping approach for the synthesis of tracking errors and Lyapunov functions, a sliding mode controller is developed in order to… 

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References

SHOWING 1-10 OF 23 REFERENCES
Feedback linearization and linear observer for a quadrotor unmanned aerial vehicle
TLDR
The performance and characteristics of a Luenberger observer, combined with a classical polynomial controller and applied to a quadrotor UAV are analyzed and shown to be efficient when dealing with bounded uncertainties and disturbances.
Attitude stabilization of a four-rotor aerial robot
TLDR
The proposed quaternion-based feedback control scheme for exponential attitude stabilization of a four-rotor vertical take-off and landing (VTOL) aerial robot known as the quadrotor aircraft shows that the model-independent PD controller provides asymptotic stability for the problem.
Backstepping and Sliding-mode Techniques Applied to an Indoor Micro Quadrotor
TLDR
The results of two nonlinear control techniques applied to an autonomous micro helicopter called Quadrotor are presented, a backstepping and a sliding-mode techniques.
Nonlinear control of underactuated mechanical systems with application to robotics and aerospace vehicles
TLDR
This main contribution is to find explicit change of coordinates and control that transform several classes of underactuated systems into cascade nonlinear systems with structural properties that are convenient for control design purposes.
Global Stabilization of the PVTOL: Real-Time Application to a Mini-Aircraft
We present a simple non-linear controller based on Lyapunov analysis for a planar vertical take-off and landing aircraft (PVTOL). It is proved that the proposed control scheme is globally
Design and control of an indoor micro quadrotor
TLDR
The approach that the lab has taken to micro VTOL evolving towards full autonomy is described, and the mechanical design, dynamic modelling, sensing, and control of the indoor VTOL autonomous robot OS4 are presented.
Dynamic modelling and configuration stabilization for an X4-flyer
Abstract A model for the dynamics of a four rotor vertical take-off and landing (VTOL) vehicle known as an X4-flyer is proposed. The model incorporates the airframe and motor dynamics as well as
Modeling, Identification and Control of Robots
World Academy of Science, Engineering and Technology 38 2010 A Numerical Study on Thermal Dissociation of
    ...
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