Hybrid high-order sliding mode-based control for multivariable cross-coupling systems: Scale-laboratory helicopter system application

被引:7
作者
Kada, B. [1 ]
Juhany, K. A. T. [1 ]
Balamesh, A. S. A. [2 ]
机构
[1] King Abdulaziz Univ, Dept Aeronaut Engn, Jeddah, Saudi Arabia
[2] King Abdulaziz Univ, Dept Elect & Comp Engn, Jeddah, Saudi Arabia
关键词
cross-coupled control; hybrid sliding mode control; helicopter control application; high-order sliding mode; nonlinear multivariable systems; robust control; MISSILE GUIDANCE; DELAY SYSTEMS; DESIGN;
D O I
10.1017/aer.2017.57
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper presents a high-order slidingmode approach to design variable structure controllers for nonlinear multivariable cross-coupling systems whereby a change in either control input affects the control loops of all the subsystems dynamics. A hybrid-sliding mode control (hybrid-SMC) scheme is constructed combining a new equivalent control algorithm with a high-order discontinuous control algorithm to benefit from the advantages of both control strategies. The hybrid-SMC scheme uses weighting coefficients to weight and combine controllers. The equivalent control algorithm uses a relative degree concept through dynamic constraints imposed on the sliding variables to overcome the limitations of the conventional approaches and to provide an optimum tracking performance. A scale-laboratory helicopter model is used to sum up the main features and demonstrate the effectiveness of the developed control scheme. The proposed hybrid-SMC strategy is compared to existing sliding modebased control approaches in terms of tracking performance, stability and control efforts. The obtained results demonstrate the validity and efficiency of the proposed hybrid-SMC scheme.
引用
收藏
页码:1319 / 1341
页数:23
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