A Design Based on SysML for High Lift System of Civil Aircraft

Xiaoyi Wang, Weida Wang, X. Cai
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Abstract

With evolution of advanced technologies and new design concepts, new functions and complex interactions are introduced into High Lift System (HLS), which cause requirements to be captured difficultly and system architecture unable to be determined through traditional documents/text to capture requirements and present system architecture, especially iterative revise on requirements and scheme will lead to system design confusion. An effective method of MBSE based on SysML has been required and applied in design of engineering field, such as an aircraft of China. This paper provides a design method based on MBSE using SysML to build up system/product architecture of High Lift System installed on aircraft from capturing demands of stakeholders to final system/products, which also considers effects on establishment of system/product taken safety as an example. This step-by-step design method can make system design and design process clear and reliable, and provide favorable support for the future validation and verification of High Lift System installed on aircraft.
基于SysML的民用飞机大升力系统设计
随着先进技术和新的设计理念的发展,高升力系统(High Lift System, HLS)中引入了新的功能和复杂的交互,导致需求捕获困难,系统架构无法通过传统的文档/文本来捕获需求和呈现系统架构,特别是对需求和方案的反复修改会导致系统设计混乱。一种有效的基于SysML的MBSE设计方法已经在工程领域得到了应用,例如中国的某型飞机。本文提出了一种基于MBSE的设计方法,利用SysML从获取利益相关者的需求到最终的系统/产品构建飞机高升力系统的系统/产品架构,并以安全为例考虑了对系统/产品构建的影响。这种分步设计方法可以使系统设计和设计过程清晰可靠,为今后高升力系统在飞机上的验证和验证提供有利的支持。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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