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Backstepping-Based Nonlinear RISE Feedback Control for an Underactuated Quadrotor UAV Without Linear Velocity Measurements

  • Jawhar GhommamEmail author
  • Luis F. Luque-Vega
  • Maarouf Saad
Chapter
Part of the Studies in Systems, Decision and Control book series (SSDC, volume 175)

Abstract

In this paper, a robust three dimensional output feedback control problem is proposed for a 6-degrees-of-freedom model of a quadrotor unmanned aerial vehicle (UAV) to track a bounded and sufficiently smooth reference trajectory in the presence of slowly varying force disturbances. Due to the underactuation structure of the UAV, a nonlinear output feedback controller based on the robust integral of the sign error signal (RISE) mechanism is first designed for the translational dynamics to ensure position reference tracking without velocity measurement. The angular velocity is then regarded as intermediate control signal for the rotational dynamics to fulfill the task of attitude angle reference tracking. The torque input is designed taking full advantage of the smooth exact differentiator that circumvents derivatives computation of virtual controls, the backstepping technique is then judiciously modified to allow the use of the RISE control technique to compensate for the external disturbances. The proposed controller yields semi-global asymptotic stability tracking despite the added disturbances in the dynamics. Simulation results are shown to demonstrate the proposed approach.

Keywords

RISE-backstepping Exact differentiator Underactuated quadrotor Output feedback 

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Copyright information

© Springer Nature Singapore Pte Ltd. 2019

Authors and Affiliations

  • Jawhar Ghommam
    • 1
    Email author
  • Luis F. Luque-Vega
    • 2
  • Maarouf Saad
    • 3
  1. 1.Department of Electrical and Computer Engineering, College of EngineeringSultan Quaboos UniversityMuscatOman
  2. 2.CIIDETEC-UVMUniversidad del Valle de MexicoMexico CityMexico
  3. 3.Department of Electrical EngineeringÉcole de Technologie SuperieureMontrealCanada

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