ABSTRACT
In this paper, an automatic measurement and control system is designed and developed for thermal vacuum test of spacecraft components. The system is built based on industrial Ethernet, with distributed measurement and control computer and unified data server as the main body to carry out test business data processing and storage, temperature data acquisition and PID closed-loop control by driving program control power supply, data acquisition instruments and other equipment, the system has strong scalability, high stability, high control accuracy, and short acquisition and control cycle. Through automatic control strategy and abnormal alarm mechanism, the system improves the ability of automatic measurement and control and abnormal handling, reduces the labor intensity of test personnel, and improves the quality control level of test process. Hundreds of thermal vacuum tests of spacecraft components have been completed by using this system, which has high application value.
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Index Terms
- Design and application of automatic measurement and control system for thermal vacuum test of spacecraft components
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