A Universal Test System Framework and Its Application on Satellite Test

Author(s):  
Xiuhai Cui ◽  
Yu Peng ◽  
Xiyuan Peng
2013 ◽  
Vol 284-287 ◽  
pp. 2371-2374
Author(s):  
Jian Dong Zhang ◽  
En Long Cao ◽  
Yong Wu ◽  
Guo Qing Shi

In modern combat aircrafts, avionics integrated systems play an increasingly important role. Bus test and analysis system is used as a testing platform for the testing, debugging, maintenance and monitoring of airborne electronic equipment, which could rapidly detect and identify the working status of the bus. This paper discusses the general avionics data bus test system design and implementation, which focuses on the test system design, system management, software development, and the bus information flow management of the whole system. The universal test and analysis system is based on the bus test analysis platform of ICD database that can effectively test ARINC429 bus and 1553B bus. Through integrating the platform into the simulation system, it can complete the closed-loop test of the integrated avionics simulation test system, analyze the state changes of various information flows during the process of bus communication, test and verify the active status and logical sequence of avionic fire control test systems, which has achieved very good results in the practical engineering applications.


2011 ◽  
Vol 462-463 ◽  
pp. 961-966
Author(s):  
Kyung Seok Oh ◽  
Kwang Hwan Oh ◽  
Jun Ho Jang ◽  
Kyung Seop Han

Universal test method to evaluate sheet metal formability was developed using finite element method based on axiomatic design. The newly developed formability test intended to generate the various modes of deformation and to control the onset of failure independently under each mode of deformation. The functional requirements (FRs) and the design parameters (DPs) of the test system were defined on axiomatic design approach and decomposed until the design reaches final stage. The independence axiom was applied throughout the design process to maintain the hierarchical independence of the formability test system. The flow diagram representing the system architecture was introduced after decomposition to give a help to establish the systematic design procedures and to determine the design parameters. Numerical simulation was carried out to determine the specific value of DPs which satisfies the FRs. Numerical results showed that modes of deformation varies accompanying various strain paths and good controllability of sheet forming is obtained for different kinds of materials. Experimental work was finally conducted to validate the proposed design. Stamping results represented that the outcome of the deformed geometry and strains are in good agreement with the numerical results.


Author(s):  
Richard C. Pitwon ◽  
Marika Immonen ◽  
Henning Schroeder ◽  
Marcel Neitz ◽  
Kai Wang

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