基于MBSE的民机审定试飞场景设计

doi:10.3969/j.issn.1001-506X.2020.08.17

Abstract

Abstract:

The flight test for airworthiness certification is a high-risk and high-cost important forensic activity to verify that the civil aircraft meets the design requirements, demonstrates the compliance with the airworthiness clauses, and forms the certification evidence. Defining and designing the test flight scenario of civil aircraft certification is a prerequisite for conducting airworthiness certification flight test. The design method and process of the certification test flight scenario based on the airworthiness compliance evidence link are then proposed. Taking "compliance evidence link" as the core, the logical and traceable airworthiness compliance evidence is planned. The model-based systems engineering (MBSE) method is introduced to realize the modeling of the process of constructing the compliance evidence link for the certification test flight scenario. In order to improve the operability, taking the airworthiness requirement "ground heading maneuverability" as a typical case, the process of requirement analysis, design, and requirement confirmation of the certification test flight scenario are demonstrated. The final designed certification test flight scenario can support the conduction of the civil aircraft airworthiness certification flight test.

Key words: model-based systems engineering (MBSE), compliance evidence link, civil aircraft airworthiness, certification test flight scenario

CLC Number:

Zhiwei MAO, Zhanwen QU, Tong ZHANG, Yi LU, Shan FU, Dan HUANG. Design of civil aircraft certification test flight scenario based on MBSE[J]. Systems Engineering and Electronics, 2020, 42(8): 1768-1775.

Figures/Tables 10

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References 27

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ATA章节	CCAR-25部适航条款
ATA章节	B分部	D分部	F分部
ATA-140	-	-	25.143 1 25.143 5
ATA-240	-	-	25.130 1 25.130 9 25.143 1
ATA-290	-	-	25.130 1 25.130 9 25.143 5
ATA-310	-	-	25.130 1 25.130 9
ATA-320	25.233(c) 25.237	25.771	25.130 1 25.130 9 25.143 5
ATA-420	25.233(c) 25.237	-	-
ATA-460	-	-	25.130 1 25.130 9

构成要素	要素描述
试飞机组	机组3人、状态正常、按流程执行任务
飞机因素	小重量、后重心、其他构型正常前轮转向系统控制飞机转向指令单点故障/单发失效电源系统负载/液压系统负载
试飞环境	白天、目视无障碍、干跑道、无异物干扰任何方向的风速小于等于5 kn
试飞流程	图6

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Design of civil aircraft certification test flight scenario based on MBSE

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