Abstract

This paper presents the design of a sliding mode control (SMC) for trajectory tracking of an unmanned aerial vehicle (UAV), quadrotor. A simplified model of the quadrotor is used for the controller design. The robustness of the controller is verified through simulations, and also through data analysis from the experiments in the 3DR Arducopter platform. The SMC algorithms are implemented in a microcontroller that communicates with a human machine interface (HMI), which monitors the behavior and stability of the state variables. The results show effectiveness of the control technique for maintaining stability in the quadrotor under different operating scenarios.

Original languageEnglish
Article number7530409
Pages (from-to)2157-2166
Number of pages10
JournalIEEE Latin America Transactions
Volume14
Issue number5
DOIs
StatePublished - May 2016

Keywords

  • nonlinear system
  • sliding mode control
  • trajectory tracking
  • unmanned aerial vehicle

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