2020
DOI: 10.1177/0142331220980274
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Coordinated optimization control of shield machine based on dynamic fuzzy neural network direct inverse control

Abstract: During shield machine tunneling, the earth pressure in the sealed cabin must be kept balanced to ensure construction safety. As there is a strong nonlinear coupling relationship among the tunneling parameters, it is difficult to control the balance between the amount of soil entered and the amount discharged in the sealed cabin. So, the control effect of excavation face stability is poor. For this purpose, a coordinated optimization control method of shield machine based on dynamic fuzzy neural network (D-FNN)… Show more

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Cited by 9 publications
(3 citation statements)
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“…Thus, the time series of construction data is established. A prediction model expression, as shown in equation (11).…”
Section: Constructing Time Seriesmentioning
confidence: 99%
See 1 more Smart Citation
“…Thus, the time series of construction data is established. A prediction model expression, as shown in equation (11).…”
Section: Constructing Time Seriesmentioning
confidence: 99%
“…Xuanyu Liu [10] proposed an intelligent online prediction of the rotation speed of the Earth pressure balance shield screw machine based on convolutional neural networkgate recurrent unit (CCN-GRU) and controlled the sealed cabin pressure by predicting the screw conveyor speed. In order to further improve the accuracy of the control effect, a dynamic fuzzy neural network (D-FNN) control system is established to output screw conveyor speed and propulsion speed at the next moment, which further improves the control effect on the sealed cabin pressure [11]. Kong Xiangxun [12] proposed a prediction method based on random forest and selected geological conditions and shield operation data as features to establish a prediction model to achieve thrust prediction.…”
Section: Introductionmentioning
confidence: 99%
“…In view of the strong coupling between channels and highly nonlinear characteristics of UAV, dynamic inverse control is used to cancel the nonlinearity of the controlled object itself [33], which requires that the mathematical model of the aircraft should be accurate. In the actual flight environment, the inverse errors are affected by the disturbance of the external turbulent wind and the uncertainty of the model, which will lead to the inability to completely cancel the nonlinearity.…”
Section: Control System Designmentioning
confidence: 99%