Quantized feedback control for a class of uncertain linear systems via supervisory-based sliding mode control

2014 ◽  
Author(s):  
Yan-Mei Xue ◽  
Li-Ping Yin ◽  
Bo-Chao Zheng
Keyword(s):  
Feedback Control ◽  
Sliding Mode Control ◽  
Linear Systems ◽  
Sliding Mode ◽  
Quantized Feedback ◽  
Mode Control ◽  
Uncertain Linear Systems

scholarly journals SLIDING MODE CONTROL OF UNCERTAIN LINEAR SYSTEMS BASED ON A HIGH GAIN OBSERVER FREE OF PEAKING

2005 ◽  
Vol 38 (1) ◽  
pp. 717-722
Author(s):  
José Paulo ◽  
V.S. Cunha ◽  
Liu Hsu ◽  
Ramon R. Costa ◽  
Fernando Lizarralde
Keyword(s):  
Sliding Mode Control ◽  
Linear Systems ◽  
Sliding Mode ◽  
High Gain ◽  
Mode Control ◽  
High Gain Observer ◽  
Uncertain Linear Systems

scholarly journals High Order Sliding-mode Control of Uncertain Linear Systems

1999 ◽  
Vol 32 (2) ◽  
pp. 3629-3634
Author(s):  
Y.A. Jiang ◽  
T. Hesketh ◽  
D.J. Clements
Keyword(s):  
Sliding Mode Control ◽  
Linear Systems ◽  
Sliding Mode ◽  
High Order ◽  
Mode Control ◽  
Uncertain Linear Systems

scholarly journals Dynamic output feedback sliding mode control for uncertain linear systems

2021 ◽  
pp. 014233122110507
Author(s):  
Jiehua Feng ◽  
Dongya Zhao ◽  
Xing-Gang Yan ◽  
Sarah K Spurgeon
Keyword(s):  
Sliding Mode Control ◽  
Linear Systems ◽  
Output Feedback ◽  
Sliding Mode ◽  
Sliding Surface ◽  
Mode Control ◽  
Sliding Motion ◽  
System Output ◽  
The Stability ◽  
Uncertain Linear Systems

In this paper, a class of uncertain linear systems with unmatched disturbances is considered, where the nominal system representation is allowed to be non-minimum phase. A sliding surface is designed which is dependent on the system output, observed state, and estimated uncertain parameters. A linear coordinate transformation is introduced so that the stability analysis of the reduced-order sliding mode dynamics can be conveniently performed. A robust output feedback sliding mode control (OFSMC) is then designed to drive the considered system state to reach the sliding surface in finite time and maintain a sliding motion thereafter. A simulation example for a high incidence research model (HIRM) aircraft is used to demonstrate the effectiveness of the proposed method.

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