System identification and uncertainty modeling of an electromechanical actuator

Salloum, Rafik; Arvan, Mohammad Reza; Moaveni, Bijan

doi:10.1080/02533839.2015.1005026

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Cited by 6 publications

(1 citation statement)

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“…The controller design of electromechanical actuators is widely researched. [13][14][15] However, there are fewer studies concerning the electromechanical actuator controller of spinning missiles. To guarantee the stability of spinning missiles, the key requirement for the actuator controller is the resistance to a sinusoidal hinge moment.…”

Section: Introductionmentioning

confidence: 99%

Retuning the actuator proportional–integral–derivative controller of spinning missiles

Zhou

Yang

Zhao

2016

Proceedings of the Institution of Mechanical Engineers, Part G:

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The hinge moment acting on the actuator will cause an out-of-plane moment, which is a destabilizing factor to the angular motion of spinning missiles. A new tuning criterion for the actuator controller is proposed to decrease the out-of-plane moment. It is noted that the integral element does not decrease the out-of-plane moment. A carefully designed proportional–derivative controller with some compromises can ensure the stability of the missile and provide good performance for the actuator.

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Section: Introductionmentioning

confidence: 99%

Retuning the actuator proportional–integral–derivative controller of spinning missiles

Zhou

Yang

Zhao

2016

Proceedings of the Institution of Mechanical Engineers, Part G:

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Modeling and identification of the multi-axis drive system using support vector machine and granular computing

Zhang

2016

Journal of the Chinese Institute of Engineers

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Adaptive Fuzzy Filter-based L ₁ Adaptive Controller Design for Electromechanical Actuator Containing Uncertainties and Disturbances

Maiti,

Sharma,

Sarkar

2024

IETE Journal of Research

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System identification and uncertainty modeling of an electromechanical actuator

Cited by 6 publications

References 18 publications

Retuning the actuator proportional–integral–derivative controller of spinning missiles

Retuning the actuator proportional–integral–derivative controller of spinning missiles

Modeling and identification of the multi-axis drive system using support vector machine and granular computing

Adaptive Fuzzy Filter-based L ₁ Adaptive Controller Design for Electromechanical Actuator Containing Uncertainties and Disturbances

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System identification and uncertainty modeling of an electromechanical actuator

Cited by 6 publications

References 18 publications

Retuning the actuator proportional–integral–derivative controller of spinning missiles

Retuning the actuator proportional–integral–derivative controller of spinning missiles

Modeling and identification of the multi-axis drive system using support vector machine and granular computing

Adaptive Fuzzy Filter-based L 1 Adaptive Controller Design for Electromechanical Actuator Containing Uncertainties and Disturbances

Contact Info

Product

Resources

About

Adaptive Fuzzy Filter-based L ₁ Adaptive Controller Design for Electromechanical Actuator Containing Uncertainties and Disturbances