scholarly journals Cascade Control System Design and Stability Analysis for a DC–DC Boost Converter with Proportional Integral and Sliding Mode Controllers and Using Singular Perturbation Theory

2021 ◽  
Author(s):  
Sajad Azarastemal ◽  
Mohammad Hejri
Keyword(s):  
Perturbation Theory ◽  
Control System ◽  
Stability Analysis ◽  
Singular Perturbation ◽  
System Design ◽  
Sliding Mode ◽  
Singular Perturbation Theory ◽  
Control System Design ◽  
Sliding Mode Controllers ◽  
Cascade Control System

Vehicle ABS control system design via integral sliding mode

2016 ◽  
Vol 10 (4) ◽  
pp. 356
Author(s):  
Shibly A. Al Samarraie ◽  
Mohsin N. Hamzah ◽  
Yasir K. Al Nadawi
Keyword(s):  
Control System ◽  
System Design ◽  
Sliding Mode ◽  
Control System Design ◽  
Integral Sliding Mode

Dynamic Anti-Windup Design for Missile Overload Control System

2012 ◽  
Vol 236-237 ◽  
pp. 273-277 ◽  
Author(s):  
Xian Jun Shi ◽  
Hong Chao Zhao ◽  
Ke Wen Xu
Keyword(s):  
Control System ◽  
System Design ◽  
Actuator Saturation ◽  
Sliding Mode ◽  
Control System Design ◽  
Sliding Mode Controller ◽  
Overload Control ◽  
Saturation Time ◽  
Simulation Results ◽  
Saturation Phase

The former research on the overload control system of a supersonic missile didn’t consider actuator saturation. In order to reduce the windup effect caused by actuator saturation, we developed a dynamic anti-windup compensator. The overload control system design adopted a two-step approach. Firstly a sliding mode controller was designed ignoring the saturation. Secondly a dynamic anti-windup compensator was designed. It added to the control system to reduce the windup effect. It disengaged the actuator fast from saturation phase after the actuator entered saturation. Simulation results showed that the dynamic anti-windup compensator reduced 52% of saturation time of the control system. Hence the performance of the overload control system is improved effectively.

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