Pitch and yaw motion control of 2 DoF helicopter subjected to faults using sliding-mode control

• Autorzy: Raghappriya M. , Kanthalakshmi S.

Identyfikatory

DOI

10.24425/acs.2022.141716

• Języki publikacji: EN

Abstrakty

EN

This paper presents a fault-tolerant control scheme for a 2 DOF helicopter. The 2 DOF helicopter is a higher-order multi-input multi-output system featuring non-linearity, cross-coupling, and unstable behaviour. The impact of sensor, actuator, and component faults on such highly complex systems is enormous. This work employs sliding mode control, which is based on reaching and super-twisting laws, to handle the problem of fault control. Simulation tests are carried out to show the effectiveness of the algorithms. Various performance metrics are analyzed and the results show SMC based on super-twisting law provides better control with less chattering. The stability of the closed-loop system is mathematically assured, in the presence of faults, which is a key contribution of this research.

Słowa kluczowe

EN

fault tolerant control; sliding mode control; reaching law; super-twisting; sensor; actuator faults; component faults

• Wydawca: Polish Academy of Sciences, Committee of Automatic Control and Robotics
• Czasopismo: Archives of Control Sciences
• Rocznik: 2022
• Tom: Vol. 32, No. 2
• Strony: 359--381
• Opis fizyczny: Bibliogr. 21 poz., fot., rys., tab., wykr., wzory

Twórcy

autor

Raghappriya M.

• Department of Electronics and Instrumentation Engineering, Government College of Technology, Coimbatore, India

autor

Kanthalakshmi S.

• Department of Electrical and Electronics Engineering, PSG College of Technology, Coimbatore, India

Bibliografia

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Uwagi

Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023)