Project Background

A research institute of China Aerospace Science and Technology Corporation (CASC) is mainly engaged in the development and production of space vehicle payload and electronic systems and equipment, vehicle measurement and control, weapons and satellite application electronic systems and equipment, as well as the research of corresponding electronics. equipment and satellite application electronic systems and equipment development, production, as well as the corresponding electronics research, strong technical force, complete professional support, advanced infrastructure, for China's space industry, national defense construction and national economic construction has made significant contributions. With strong technical force, complete professional support and advanced infrastructure, it has made significant contributions to China's space industry, national defense construction and national economic construction.

 

Project Design

The system is mainly used for XX antenna impact test, mainly to complete the XX test force, vibration and other dynamic and static parameters of the acquisition and analysis. The system is mainly used for the XX antenna impact test, and it can collect and analyze the dynamic and static parameters of force and vibration in the XX test. Requirements for equipment structure is compact, stable and reliable, adapt to the field test environment, the system is practical for the purpose; to facilitate the test analysis, Improve the efficiency of the system, shorten the test analysis cycle for the direction; can realize the test process sensor excitation, signal conditioning, to meet the data Recording, analysis and processing and analysis and calculation of various test state performance parameters, and real-time display of test curves, real-time preservation of test test data; output test data on request The test data can be output according to the requirements of the test report, which can be further used for the verification, correction and improvement of the XX antenna unfolding impact force.

 

System composition

The XX antenna unfolding impact test system includes 1 set of TRIONET, a portable host, a multifunctional acquisition module (signal conditioning, A/D conversion integrated multifunctional), a multifunctional acquisition module (signal conditioning, A/D conversion integrated multi-function module) TRION-2402-MULTI series of 3 blocks, MSI charge adapter 20, a dedicated computer. American PCB company triaxial force sensor (IEPE type) M261A024 sets, JiangSu Luneng triaxial force sensor (charge type) CL - YD-3310 series 6 sets. YD-3310 series 6 units, charge amplifier YE58533 units, as well as random cables and other accessories.