2022
DOI: 10.11591/ijece.v12i5.pp4883-4891
|View full text |Cite
|
Sign up to set email alerts
|

Robust control for a tracking electromechanical system

Abstract: <p>A strategy for the design of robust control of tracking electromechanical systems based on 𝐻∞ synthesis is proposed. Proposed methods are based on the operations on frequency characteristics of control systems designed and developed using the MATLAB robust control toolbox. Determination of the singular values for a transfer matrix of the control system reduces the disturbances and guarantees its stability margin. For selecting the weighted transfer functions, the basic recommendations are formulated.… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2023
2023
2023
2023

Publication Types

Select...
1

Relationship

0
1

Authors

Journals

citations
Cited by 1 publication
(1 citation statement)
references
References 16 publications
0
1
0
Order By: Relevance
“…Beisenbi and Basheyeva [29] describes the application of the Lyapunov function to construct robustly stable aircraft control systems. Karimtaevna and Asylbekkyzy [30] outlines a design methodology and implementation of robust control using H∞ synthesis tools, which allows to cope more effectively with parameters and load perturbation. The research conducted in Karimtaevna et al [31] delves into a meticulous investigation of the H2 and H∞ synthesis methods, specifically exploring their potential in the realization systems responsible for controlling the flight of an aircraft during the crucial landing phase, while effectively mitigating the impact of external disturbances.…”
Section: Introductionmentioning
confidence: 99%
“…Beisenbi and Basheyeva [29] describes the application of the Lyapunov function to construct robustly stable aircraft control systems. Karimtaevna and Asylbekkyzy [30] outlines a design methodology and implementation of robust control using H∞ synthesis tools, which allows to cope more effectively with parameters and load perturbation. The research conducted in Karimtaevna et al [31] delves into a meticulous investigation of the H2 and H∞ synthesis methods, specifically exploring their potential in the realization systems responsible for controlling the flight of an aircraft during the crucial landing phase, while effectively mitigating the impact of external disturbances.…”
Section: Introductionmentioning
confidence: 99%