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Published byMagnus Marshall Modified over 9 years ago
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Progress Report on CGSE Control System Project Team of SJTU for AMS-02 Yang Yupu AMS TIM @NASA JSC, Jan 8-12, 2007
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I/O Module PROFIBUS PLC Cryostat valves Box Dewar system Monitoring PC operator station MagnetCAB CGSE = Cryogenic Ground Support Equipment ( Cryo-magnet Avionics Box) Tasks of CGSE 1 Cooling down the AMS magnet (from 300K to 1.8K) 2 Filling magnet vessel with super-fluid helium (~2500 lit @1.8 K ) CANbus
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Contents 1 Hardware System Completed 2 Software Modules are Ongoing 2.1 Communicating Module 2.1 Communicating Module 2.2 Control Algorithm Module 2.2 Control Algorithm Module 2.3 HMI Module 2.3 HMI Module 3 Test 3 Test Platform for Super-fluid Helium Experiment 4 Further Works
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1 Hardware System Completed 1.1 Config of S7-410H controller is finished 1.2 Config of ET200-DP stations is finished 1.3 Hardware of Communication is finished 1.3 Hardware of Communication is finished
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Hardware System Completed Redundant Controller Distributed I/O Module Communication Interface Magnet Data Simulator CGSE-Valve Control simulator
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Assembly of the Redundant PLC System in SJTU Redundant PLC WinCC HMI Distributed I/O Module Redundant Frofibus
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Config of S7-414H PLC Structure Config PLC 414H Config Field-Bus Config
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Distributed I/O Module: Siemens ET-200
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2.1 Communicating Module 1 Communicating Module based on CANbus
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I/O Module PROFIBUS PLC Cryostat valves Box Dewar system Monitoring PC operator station MagnetCAB CGSE = Cryogenic Ground Support Equipment ( Cryo-magnet Avionics Box) Tasks of CGSE 1 Cooling down the AMS magnet (from 300K to 1.8K) 2 Filling magnet vessel with liquid helium (~2500 lit @1.8 K ) CANbus
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CGSE control system need to get from the magnet the following parameters (Confirmed at the TIM@cern April 2006) 1.Temperatures of helium cooling flow across the magnet T21, T19 and their difference (T21-T19). (from CAB) (This temperature difference should be not more 50 K during cooling of the magnet in the range 300-80 K ) 2. Helium temperature T07. (from CAB) ( for control of pumping AMS magnet to super fluid state at 1.8 K ) following parameters for filling up procedure: 3. Signal from helium level meters L02, L03. (CGSE direct from the meters) 4. Pressure in AMS main helium tank P04, P05. (from CAB) 5. Temperatures of the AMS VCS T09-T12. ( from CAB) 6. AMS temperatures in SFHe Cooling Loop (T01-T06). (from CAB ) 7. Position of AMS valves: open or close. (Some from CAB, some from CGSE and new table from SCL/McMahon 5 May,2006)
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CAN Master CAN Master Port Socket Server Port Command and Data Transmitting CAN Slave TCP_Client CAN Slave Port Socket Client port Control Command and Receive Data Response and Data CAN Net Ether Net Display Interface 1 CAN Master is mainly used at the connection and communication between CAN networks and TCP/IP networks. It functionally works as an gateway. 2 Function of TCP Client is to Simulate CGSE sending commands to TCP Server (CAN Master) through the TCP/IP networks and receiving its response. 3 CAN Slave is mainly used to simulate the slave node (CAB) of CGSE, and implement the functions such as data-feedback, reading the values of locale data- collection equipment, etc. Function of CAN Master, TCP_Client and CAN Slave 1 Communicating Module based on CANbus
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Display Interface of CAN_Slave Display Interface of CAN Master Display Interface of TCP Client
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Testing of communication software in SJTU CAN Master TCP_Client CAN Slave (CAB of Magnet) Interface of CGSE-MS Ethernet FrofiBus
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EPP-CAN Boxes and temperature sensor in communication software testing EPP-CAN Box1 EPP-CAN Box2 CAN Bus Sensor Transmeter
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2.1 Communicating Module 2.1 Communicating Module 2 Communicating Module 2 Communicating Module for CAB
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CAB CAN Ethernet CAB Simulator (Linux) FEP Magnet_server / CAB_Master Server socket FEP Client socket AMS Block CAB Commands Server socket Magnet Data (Windows) Magnet Client OPC Win CC & Other Modules EPP-CAN Box Magnet CAB Slave CAN Port Magnet Client socket Communicating Module General Scheme of Communicating Module for CAB
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CGSE-Magnet Date CAB Commands BeforeAfter CGSE- Magnet Date Data format used in the module
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Developing work is ongoing
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2.2 Control Algorithm Module 1 Supervising of Status of I/O Stations 2 Testing PID Control Algorithm of Valves 3 Test Module for OPC Link 4 Object Identification Module 5 Control test for large Delay Temperature Process 6 Modified Smith Control Algorithm
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1 Supervising of Status of I/O Stations
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2 Testing PID Control Algorithm of Valves
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OPC Interaction Module Functions Diagram of OPC Interaction Module Communication Based on OPC 3 Test Module for OPC Link OPC is a important protocol used in control industry for easy linking software which produced by different developers.
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4 Object Identification Module y(k)= 0.7093y(k-1) + 0.1260y(k-2)+0.1619y(k-3) +0.0007u(k-15)+ 0.0038u(k-16) Identification Algorithm Identification Result Identification Object Identification Data
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5 Control test for large Delay Temperature Process Control with a high precision for a large delay object is still a challenge in control community. The process of cooling down the Magnet is maybe a large delay control task.
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Control test to large Delay Temperature Process (Hardware)
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6 Modified Smith Control Algorithm Structure Diagram of Modified Smith Control System Object PID Controller Adaptive Smith Predictor Output of Predictor (Smith Control Algorithm is a basic method to control delay object, but it is difficult to satisfy for large delay object.)
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Simulation Result of Cooling Down for the Magnet Predictive Result of Modified Smith Predictor Predictor Output Prediction Ahead Response of System with Modified Smith Predictor Standard Smith Controller Our Modified Smith Controller
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2.3 HMI Module HMI of CGSE Control System Based on Siemens WinCC
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4 Control 4 Control Platform for Super-fluid Helium Experiment In SJTU
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Design Requirement 1 Provide a control and measure system for obtaining, maintaining and transmitting super-fluid helium 2Support the function such as multi-data collecting, display, recording and archiving of the process data 3Flexible and expandable. Some functional modules in this system are designed to be suitable for other occasions in CGSE
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Measurement and Control Platform for super-fluid helium VB6 Environment WIN XP Advantech DLL Driver PCI 1620 B 8-port 232 communicating board COM1COM2COM3COM4COM5 Liquid-Level Monitor # 2 232 Temperature instrument # 2 232 Liquid-Level Monitor # 1 232 Temperature instrument # 1 232 Sensor of the pressure difference PCI 1710 AI/AO/DI/DO AI 0 COM6 ADAM4522 232 485 ADAM-4017 ADAM-4024 ADAM-4050 Flow Meter # 1 232 Hardware Schema of the Control Platform The platform is built under MCGS and VB6 environment upon an industrial computer, which communicates with instruments through PCI boards
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HMI Hardware Assembly of the Control Platform Controller Signal Connection Box
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Instrument typeQuantityInterface 1Thermometer 93504RS232 2Pressure Transducer ( MPM4730 ) 3 4~20mA , RS485 3Pressure Transducer ( MPM4760 ) 3 4~20mA , RS485 4Pressure difference Transducer ( MDM4951 ) 14~20mA 5Pressure difference Transducer ( MDM484A ) 14~20mA 6 Liquid Level Monitor ( 135-2k ) 2 4~20mA , RS232 7 Flow Meter ( M Serial ) 4RS232 List of Signal type and interface
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Software design Object Platform design Environment Strategies design
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HMI of Control Platform for Super-fluid Helium Experiment Experiment Platform For Super-fluid Helium Differential Pressure Gas Temperature Dewar1 Liquid Temperature Liquid Level Gas Temperature Pressure Liquid Level Liquid Temperature Dewar2 Flux
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The Control Platform in the working place of Super-fluid Helium Experiment in SJTU Dewar 1 Dewar 2 Control Platform Pipeline of SF Helium Compressor
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4 Further Works 1 Continue to perfect the communication the software 2 Continue to configure the Interface between PLC and mechanical system of CGSE. 3 Continue to develop HMI (Human Machine Interface) software based on Siemens WinCC. 4 Continue to develop software modules for whole integration of CGSE in SJTU
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Thank You!
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