系统工程与电子技术(英文版)2024,Vol.35Issue(1) :242-258.DOI:10.23919/JSEE.2024.000017

Robust design of sliding mode control for airship trajectory tracking with uncertainty and disturbance estimation

WASIM Muhammad ALI Ahsan CHOUDHRY Mohammad Ahmad SHAIKH Inam Ul Hasan SALEEM Faisal
系统工程与电子技术(英文版)2024,Vol.35Issue(1) :242-258.DOI:10.23919/JSEE.2024.000017

Robust design of sliding mode control for airship trajectory tracking with uncertainty and disturbance estimation

WASIM Muhammad 1ALI Ahsan 2CHOUDHRY Mohammad Ahmad 2SHAIKH Inam Ul Hasan 1SALEEM Faisal3
扫码查看

作者信息

  • 1. Department of Aeronautics and Astronautics Engineering,Institute of Space Technology,Islamabad 44000,Pakistan
  • 2. Department of Electrical Engineering,University of Engineering and Technology,Taxila 47080,Pakistan
  • 3. Department of Measurements and Control Systems,Silesian University of Technology,Gliwice 44-101,Poland;The Joint Doctoral School,Silesian University of Technology,Gliwice 44-100,Poland
  • 折叠

Abstract

The robotic airship can provide a promising aero-static platform for many potential applications.These applica-tions require a precise autonomous trajectory tracking control for airship.Airship has a nonlinear and uncertain dynamics.It is prone to wind disturbances that offer a challenge for a trajectory tracking control design.This paper addresses the airship trajec-tory tracking problem having time varying reference path.A lumped parameter estimation approach under model uncertain-ties and wind disturbances is opted against distributed parame-ters.It uses extended Kalman filter(EKF)for uncertainty and dis-turbance estimation.The estimated parameters are used by sli-ding mode controller(SMC)for ultimate control of airship trajec-tory tracking.This comprehensive algorithm,EKF based SMC(ESMC),is used as a robust solution to track airship trajectory.The proposed estimator provides the estimates of wind distur-bances as well as model uncertainty due to the mass matrix vari-ations and aerodynamic model inaccuracies.The stability and convergence of the proposed method are investigated using the Lyapunov stability analysis.The simulation results show that the proposed method efficiently tracks the desired trajectory.The method solves the stability,convergence,and chattering prob-lem of SMC under model uncertainties and wind disturbances.

Key words

airship/chattering/extended Kalman filter(EKF)/model uncertainties estimation/sliding mode controller(SMC)

引用本文复制引用

出版年

2024
系统工程与电子技术(英文版)
中国航天科工防御技术研究院 中国宇航学会 中国系统工程学会 中国系统仿真学会

系统工程与电子技术(英文版)

CSTPCD
影响因子:0.64
ISSN:1004-4132
参考文献量35
段落导航相关论文