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Robust control for a quadrotor aircraft with small overshoot and high-precision position tracking performance

  • Published:2020-12 Issue:18 Volume:357 Page:13386-13409
  • ISSN:0016-0032
  • Container-title:Journal of the Franklin Institute
  • language:en
  • Short-container-title:Journal of the Franklin Institute

Author:

Wang Yingyang,Hu Jianbo

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Networks and Communications,Signal Processing,Control and Systems Engineering

Reference52 articles.

1. An integral predictive nonlinear control structure for a quadrotor helicopter;Raffo;Automatica,2010

2. Nonlinear and adaptive intelligent control of techniques for quadrotor UAV-a survey;Mo;Asian J. Control,2019

3. Robust quadrotor control: attitude and altitude real-time results;Ricardo;J. Intel. Robot. Syst.,2017

4. Feedback linearization vs. adaptive sliding mode control for a quadrotor helicopter;Lee;Int. J. Control Autom. Syst.,2009

5. Robust image-based control of the quadrotor unmanned aerial vehicle;Jabbari;Nonlinear Dyn.,2016

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1. Command Filter AILC for Finite Time Accurate Tracking of Aircraft Track Angle System Based on Fuzzy Logic;Advances in Mathematical Physics;2023-08-18

2. Finite-Time Height Control of Quadrotor UAVs;Applied Sciences;2023-07-06

3. Optimized reduced order ARX modelling and robust control for multivariable uncertain systems;Transactions of the Institute of Measurement and Control;2023-04-25

4. Adaptive iterative learning control method for finite-time tracking of an aircraft track angle system based on a neural network;Frontiers in Physics;2022-12-20

5. Continuous Finite-Time Sliding Mode Control for an Uncertain Coaxial Octorotor UAV;Proceedings of the 2022 4th International Conference on Robotics, Intelligent Control and Artificial Intelligence;2022-12-16
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