-
1.发明公开
公开(公告)号：EP4460832A1
公开(公告)日：2024-11-13
申请号：EP23715766.4
申请日：2023-03-20
-
-
公开(公告)号：EP4002023B1
公开(公告)日：2024-09-25
申请号：EP20844633.6
申请日：2020-06-04
CPC分类号： C21B2300/0420130101 , C21B5/006 , G05B13/0265 , G06N3/08 , G06N3/048 , G06N3/045
-
公开(公告)号：EP4428636A2
公开(公告)日：2024-09-11
申请号：EP23211728.3
申请日：2023-11-23
发明人： Grefen, Kilian
CPC分类号： G05B13/04 , B25J9/1664 , G05B2219/4047420130101 , G05B2219/4051520130101 , G05B2219/3908720130101 , B25J9/1671
摘要： The present invention relates to the field of automated control process generation for control of a cyber-physical system. In more detail the present invention relates to a method of specifying a control process for a cyber-physical system and a related control process specifying engine. Control process specification is achieved by specifying at least one control process observation target to be reached by the control process. Then, according to the present invention a method of generating at least one control process instruction for the specified control process and a related control process experiment execution engine are used for automated control process generation through execution of control process experiments.
-
公开(公告)号：EP4421574A1
公开(公告)日：2024-08-28
申请号：EP24154707.4
申请日：2024-01-30
申请人： Rolls-Royce plc
发明人： Horobin, Marcus S
IPC分类号： G05B19/042 , G05B13/04
CPC分类号： G05B19/0421 , G05B2219/4101120130101 , G05B2219/4102120130101 , G05B2219/4102820130101 , G05B2219/262320130101 , G05B13/02
摘要： A computer-based control system for a gas turbine engine (10). The control system comprises: a controller (100, 100a, 100b) comprising control logic, the controller (100, 100a, 100b) configured to obtain a set of inputs formed by (i) measurements of one or more process variables (1) and (ii) values of one or more engine operation set points (3), and the control logic configured to determine one or more process command values (4) for operation of the gas turbine engine (10) in response to the set of inputs; and an event detection unit (200) configured to obtain further measurements of one or more process variables (1) and determine whether an abnormal event has occurred based on the further measurements of one or more process variables (1). The controller (100, 100a, 100b) comprises a plurality of tuning variables (5) for altering the one or more process command values (4) output by the control logic in response to a given set of inputs, the tuning variables (5) having respective standard values for normal operation of the gas turbine engine (10). The event detection unit (200) is configured to output an event accommodation data array (6) to the controller (100) when an abnormal event is detected, each element in the event accommodation data array (6) corresponding to a respective tuning variable (5) and one or more of the elements assigned intervention values for their respective tuning variables (5). The controller (100, 100a, 100b) is further configured to update the tuning variables (5) using the event accommodation data array (6), a given tuning variable (5) being changed in response to detection of a given abnormal event when the respective element in the event accommodation data array (6) is assigned an intervention value.
-
公开(公告)号：EP3749863B1
公开(公告)日：2024-08-28
申请号：EP19710599.2
申请日：2019-02-04
-
公开(公告)号：EP4276891A3
公开(公告)日：2024-08-21
申请号：EP23200925.8
申请日：2019-10-07
发明人： Banna, Samer , Cantwell, Dermot , Bishara, Waheb , Engel, Lior
IPC分类号： G05B13/04 , G05B19/418 , H01L21/67
CPC分类号： G05B19/41875 , G05B2219/3722420130101 , Y02P90/02 , G05B2219/3219420130101 , G05B2219/3219320130101
摘要： A spatial model is built to predict performance of a processing chamber. The spatial model is used to converge faster to a desired process during the process development phase. A system for controlling device performance variability during manufacturing includes a process platform, on-board metrology (OBM) tools, and a machine-learning based process control model. The system receives SEM metrology data, and updates the process control model periodically (e.g., wafer-to-wafer, lot-to-lot, chamber-to-chamber etc.) using machine learning techniques. Periodic update of the process control model may account for chamber-to-chamber variability.
-
8.发明公开
公开(公告)号：EP4405622A1
公开(公告)日：2024-07-31
申请号：EP22922617.0
申请日：2022-01-25
申请人： Siemens Schweiz AG
发明人： GUAN, Jin Yan , QU, Ying , FENG, Cheng , LIU, Xiao Nan
CPC分类号： F24F11/62 , G05B13/042 , G05B15/02 , G05B2219/261420130101 , F24F2130/1020180101 , F24F11/64 , F24F11/47
-
-
公开(公告)号：EP4350452A3
公开(公告)日：2024-07-10
申请号：EP24159551.1
申请日：2018-08-08
申请人： The Boeing Company
CPC分类号： G05B13/048 , B64C13/505
摘要： Systems for compensating for force fighting in multi-actuator systems are provided. A drive controller unit comprises a first feedforward controller in communication with a first actuator and configured to receive a drive command signal. A first feedback regulator is configured to output a first feedback input into the first feedforward controller, and to receive as input a first actuator position and a first actuator force. The drive controller unit further comprises a second feedforward controller in communication with a second actuator and configured to receive the drive command signal. A second feedback regulator is configured to output a second feedback input into the second feedforward controller, and to receive as input a second actuator position and a second actuator force. The drive controller unit utilizes both feedforward controllers and both feedback regulators to minimize force fighting while driving a common control surface of an aircraft.
-
-
-
-
-
-
-
-
-
搜索结果
2197 条记录 (耗时 0.023 秒)
