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Modular Design Method of Integrated Avionics Simulation System

机译:集成航空电子仿真系统的模块化设计方法

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? 2019, The Editorial Board of Journal of System Simulation. All right reserved. ? 2019, The Editorial Board of Journal of System Simulation. All right reserved. In the past, there were some problems in the software design for the flight simulation avionics system such as the decentralized structure and the low degree of modularization. Aiming at these problems, a hierarchical, modular integrated avionics system is constructed. The logic part dispersed in each function module is independent to form the integrated logic module. Each task function module and its sub module are responsible for the calculation of the relevant task function algorithm. Modular design is carried out in a deeper level. By dataflow analysis, each module in this design has strong cohesion and weak coupling and strong independence. The whole design structure is reasonable; the program is understandable and readable; and the software is reliable and maintainable. In the past, there were some problems in the software design for the flight simulation avionics system such as the decentralized structure and the low degree of modularization. Aiming at these problems, a hierarchical, modular integrated avionics system is constructed. The logic part dispersed in each function module is independent to form the integrated logic module. Each task function module and its sub module are responsible for the calculation of the relevant task function algorithm. Modular design is carried out in a deeper level. By dataflow analysis, each module in this design has strong cohesion and weak coupling and strong independence. The whole design structure is reasonable; the program is understandable and readable; and the software is reliable and maintainable.
机译:还2019年,系统模拟杂志。保留所有权利。还2019年,系统模拟杂志。保留所有权利。在过去,飞行模拟航空电子系统的软件设计中存在一些问题,例如分散结构和低模块化程度。针对这些问题,构建了一个分层的模块化集成航空电子系统。分散在每个功能模块中的逻辑部分是独立的,以形成集成逻辑模块。每个任务函数模块及其子模块负责计算相关任务函数算法。模块化设计在更深层次的水平中进行。通过DataFlow分析,这种设计中的每个模块具有强大的凝聚力和弱耦合和强大的独立性。整个设计结构是合理的;该计划是可理解和可读的;并且该软件可靠和可维护。在过去,飞行模拟航空电子系统的软件设计中存在一些问题,例如分散结构和低模块化程度。针对这些问题,构建了一个分层的模块化集成航空电子系统。分散在每个功能模块中的逻辑部分是独立的,以形成集成逻辑模块。每个任务函数模块及其子模块负责计算相关任务函数算法。模块化设计在更深层次的水平中进行。通过DataFlow分析,这种设计中的每个模块具有强大的凝聚力和弱耦合和强大的独立性。整个设计结构是合理的;该计划是可理解和可读的;并且该软件可靠和可维护。

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