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Aircraft system simulation methods in recent Airbus programmes

机译:飞机系统仿真方法在最近的空中客车程序中

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The A380 programme was for AIRBUS an opportunity to establish new methods for system modelling. Compared to previous programmes, the aircraft has a larger number of system controllers and a greatly increased level of data exchange in the aircraft network. At the same time AIRBUS required their equipment suppliers to provide simulation models. This policy was intended to allow more complete models to be available on all types of simulators, increasing the overall fidelity. This paper presents the approach that was taken to improve the system modelling phase in order to face these technological changes. In this context, the following issues are discussed: 1. Modelling phase: How the fidelity of models was improved by using formal specifications of the system controllers from the AIRBUS Design Office. Development of the models with particular attention paid to respecting the aircraft equipment interface. Extension of the use of modelling tools based on logic diagrams (such as Scade or Matlab Simulink) to reduce computer programming errors and to increase the efficiency of modelling. 2. Verification phase: Use of automatic stand-alone verification and non-regression checking of the model formal specifications to consolidate the development phase and to carry out in depth checks prior to simulator integration sessions. 3. Validation phase: The same models can be used on the different A380 simulators, from the desktop simulator to the integration simulator (known as Aircraft 0), providing a high level of model maturity and fidelity very early in the Aircraft Programme (by interfacing them with real system controllers and making direct comparisons available), and before making them available for use on training simulators. The future trends of simulation solutions are also discussed, in particular the way model elements developed for the A380 simulators could be reused on forthcoming A400M and A350 simulators. Examples from the A380 Electrical and Engine simulations are used to emphasize the implementation of these methods and the levels of fidelity and maturity these models are expected to achieve.
机译:A380计划用于空中客车设立建立系统建模方法的机会。与以前的程序相比,该飞机有更多的系统控制器和飞机网络中的数据交换水平大量增加。同时空中客车需要其设备供应商提供仿真模型。此政策旨在允许更多类型的模型可在所有类型的模拟器上使用,从而提高整体保真度。本文介绍了改善系统建模阶段的方法,以面对这些技术变革。在这种情况下,讨论了以下问题:1。建模阶段:如何通过使用空中客车设计办公室的系统控制器的正式规格来改善模型的保真度。尊重飞机设备接口特别关注的模型的开发。基于逻辑图(例如SCADE或MATLAB SIMULINK)来扩展建模工具的使用,以减少计算机编程错误并提高建模效率。 2.验证阶段:使用自动独立验证和非回归检查模型正式规范以巩固开发阶段,并在模拟器集成会话之前在深度检查中进行。 3.验证阶段:可以在不同的A380模拟器上使用相同的型号,从桌面模拟器到集成模拟器(称为飞机0),在飞机程序中非常早期提供高水平的模型成熟度和保真度(通过接口它们与真实的系统控制器并提供直接比较),并在使它们可用于培训模拟器之前。还讨论了模拟解决方案的未来趋势,特别是在即将到来的A400M和A350模拟器可以重复使用为A380模拟器开发的模型元素的方式。 A380电气和发动机模拟的示例用于强调这些方法的实施以及预期这些模型的保真度和成熟程度。

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