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

被引:0
作者
WASIM Muhammad [1 ]
ALI Ahsan [2 ]
CHOUDHRY Mohammad Ahmad [2 ]
SHAIKH Inam Ul Hasan [1 ]
SALEEM Faisal [3 ,4 ]
机构
[1] Department of Aeronautics and Astronautics Engineering, Institute of Space Technology
[2] Department of Electrical Engineering, University of Engineering and Technology
[3] Department of Measurements and Control Systems, Silesian University of Technology
[4] The Joint Doctoral School, Silesian University of Technology
关键词
D O I
暂无
中图分类号
TP273 [自动控制、自动控制系统]; V274 [气艇(飞艇)]; V249 [飞行控制系统与导航];
学科分类号
080201 ; 0835 ; 082503 ; 081105 ;
摘要
The robotic airship can provide a promising aerostatic platform for many potential applications. These applications 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 trajectory tracking problem having time varying reference path. A lumped parameter estimation approach under model uncertainties and wind disturbances is opted against distributed parameters. It uses extended Kalman filter(EKF) for uncertainty and disturbance estimation. The estimated parameters are used by sliding mode controller(SMC) for ultimate control of airship trajectory 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 disturbances as well as model uncertainty due to the mass matrix variations 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 problem of SMC under model uncertainties and wind disturbances.
引用
收藏
页码:242 / 258
页数:17
相关论文
共 24 条
[1]  
Airship aerodynamic model estimation using unscented Kalman filter[J] WASIM Muhammad;ALI Ahsan; Journal of Systems Engineering and Electronics 2020, 06
[2]  
Unscented Kalman filter for airship model uncertainties and wind disturbance estimation.[J] Wasim Muhammad;Ali Ahsan;Choudhry Mohammad Ahmad;Saleem Faisal;Shaikh Inam Ul Hasan;Iqbal Jamshed PloS one 2021,
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