2022
DOI: 10.1016/j.isatra.2021.08.007
|View full text |Cite
|
Sign up to set email alerts
|

Experimental validation of optimized fast terminal sliding mode control for level system

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
0
0

Year Published

2022
2022
2024
2024

Publication Types

Select...
6
1

Relationship

0
7

Authors

Journals

citations
Cited by 7 publications
(2 citation statements)
references
References 28 publications
0
0
0
Order By: Relevance
“…For example, W. Xu et al [19] used the adaptive velocity particle swarm optimization (AVPSO) technique to optimize the control parameters of an anti-windup proportional and integral (AWPI) controller off-line. Ghogare MG et al [20] described the process control application of a single-input, single-output (SISO) level control system that uses a combination of fast terminal sliding-mode control (FTSMC) and an optimization method. Jin Z et al [21] proposed a hybrid wolf optimization algorithm (HWOA) to automatically change the controller parameters of SMDTC for SPMSMs.…”
Section: Introductionmentioning
confidence: 99%
“…For example, W. Xu et al [19] used the adaptive velocity particle swarm optimization (AVPSO) technique to optimize the control parameters of an anti-windup proportional and integral (AWPI) controller off-line. Ghogare MG et al [20] described the process control application of a single-input, single-output (SISO) level control system that uses a combination of fast terminal sliding-mode control (FTSMC) and an optimization method. Jin Z et al [21] proposed a hybrid wolf optimization algorithm (HWOA) to automatically change the controller parameters of SMDTC for SPMSMs.…”
Section: Introductionmentioning
confidence: 99%
“…However, its convergence speed becomes slower when states are far from the equilibrium point. Thus, a fast TSMC (FTSMC) method [24] has been proposed to achieve faster convergence for TSMC. In [25], this method is used to control the attitude of UAV accurately and quickly despite external disturbance, model uncertainty, and actuator faults.…”
Section: Introductionmentioning
confidence: 99%