A gain-scheduled control algorithm for input constrained systems to track time-varying references using controller state resets

2016 ◽  
Vol 12 (1) ◽  
pp. 87-95 ◽  
Author(s):  
Nobutaka Wada ◽  
Naoki Kawaoka ◽  
Masami Saeki
2013 ◽  
Vol 753-755 ◽  
pp. 2674-2678
Author(s):  
Kun Yang ◽  
Cai Jun Liu ◽  
Shu Min Liu

Based on the situation that the hydraulic position servo system is easily influenced by the external interference and the parameters of which are different with time-varying, the fuzzy control can soften the buffeting and the sliding algorithm has no the same problems as the hydraulic position servo system, a brandly-new fuzzy sliding control algorithm is designed. In the simulation process, within the parameters of simulated time-varying and outside strong interference, the results show that the hydraulic servo system based on fuzzy sliding mode control algorithm has a greater resistance to internal and external interference and time-varying parameters.


2004 ◽  
Vol 52 (9) ◽  
pp. 2464-2476 ◽  
Author(s):  
N.T. Hoang ◽  
H.D. Tuan ◽  
P. Apkarian ◽  
S. Hosoe

2021 ◽  
pp. 107754632110501
Author(s):  
Ji-Won Lee ◽  
Nguyen Xuan-Mung ◽  
Ngoc Phi Nguyen ◽  
Sung Kyung Hong

In recent years, the boom of the quadcopter industry resulted in a broad range of real-world applications which highlighted the urgent need to improve quadcopter control quality. Typically, external disturbances, such as wind, parameter uncertainties caused by payload variations, or the ground effect, can severely degrade the quadcopter’s altitude control performance. Meanwhile, widely used controllers like the proportional-integral-derivative control cannot guarantee control performance when the system is critically affected by factors that exhibit a high degree of variability with time. In this paper, an adaptive control algorithm is proposed to improve quadcopter altitude tracking performance in the presence of both the ground effect and a time-varying payload. First, we derive an adaptive altitude control algorithm using the sliding mode control technique to account for these uncertainties in the quadcopter dynamics model. Second, we apply Lyapunov theory to analyze the stability of the closed-loop system. Finally, we conduct several numerical simulations and experiments to validate the effectiveness of the proposed method.


2020 ◽  
Vol 28 (8) ◽  
pp. 1620-1630 ◽  
Author(s):  
Dapeng Li ◽  
Lei Liu ◽  
Yan-Jun Liu ◽  
Shaocheng Tong ◽  
C. L. Philip Chen

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