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Chapter 64 An Investigation of Model-Based Design Framework for Aero-Engine Control Systems

机译:第64章航空发动机控制系统基于模型的设计框架研究

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Throughout the design of aero-engine control systems, modeling and simulation technologies have been widely used for supporting the conceptualization and evaluation. Due to the increasing complexity of such systems, the overall quality management and process optimization are becoming more important. This in particular brings the necessity of integrating various domain physical models that are traditionally based on different formalisms and isolated tools. In this paper, we present the initial concepts towards a model-based design framework for automated management of simulation services in the development of aero-engine control systems. We exploit EAST-ADL and some other existing state-of-the-art modeling technologies as the reference frameworks for a formal system description, with the content ranging from requirements, to design solutions and extra-functional constraints, and to verification and validation cases, etc. Given such a formal specification of system V&V (Verification and Validation) cases, dedicated co-simulation services will be developed to provide the support for automated configuration and execution of simulation tools. For quality management, the co-simulation services themselves will be specified and managed by models in SysML.
机译:在整个航空发动机控制系统的设计中,建模和仿真技术已广泛用于支持概念化和评估。由于此类系统日益复杂,因此总体质量管理和流程优化变得越来越重要。这尤其带来了集成各种传统上基于不同形式主义和隔离工具的领域物理模型的必要性。在本文中,我们提出了基于模型的设计框架的初始概念,该模型用于在航空发动机控制系统的开发中对模拟服务进行自动管理。我们将EAST-ADL和其他一些现有的最新建模技术用作正式系统描述的参考框架,其内容范围从需求到设计解决方案和功能外约束,以及验证和确认案例给定这样的系统V&V(验证和确认)案例的正式规范,将开发专用的协同仿真服务,以提供对仿真工具的自动配置和执行的支持。对于质量管理,协同仿真服务本身将由SysML中的模型指定和管理。

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