| In recent years, with the development of virtual technology, computer technology and aviation industry, aerospace intelligent instrument has developed from the integrated system to the system centered on computer and special ground test platform. In the new system, computer is the uniform hardware platform, and software is critical to the intelligent test. This thesis has systematically studied the software and hardware architecture module of aerospace intelligent instrument, analyzed functional requirements of the software system and the problems such as big difficulty, complex process and low generality to develop the software system. In order to simplify the development process and realize the modularization, generalization and standardization of the software system, configuration technology has been used to develop the software system based on the concept of configuration software.Firstly, overall scheme of configuration system has been designed based on the principle and software requirements of aerospace intelligent instrument. Secondly, configuration software has been designed based on VB and VC. Thirdly, basic functional modules and interface parameters have been designed based on the requirements of interface configuration, equipment configuration and data processing configuration, resource libraries of the configuration system have been established and configurably used, including data processing module library, equipment module library and from module library.In this thesis, configuration system has been successfully designed according to the development requirements of aerospace intelligent instrument soft system, and configuration technology has been successfully used to research a certain missile loaded data recorder. As it is shown, the design of this configuration system satisfies the development requirements of the aerospace intelligent instrument soft system, and realizes the application of configuration technology in the aerospace intelligent test technology. |
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