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基于有限谓词追踪的民机系统需求一致性检查方法

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针对民机安全关键系统在正向研发过程中,系统级需求的正确性难以在设计早期全部完成确认的问题,提出一种基于有限谓词追踪的功能需求一致性检查体系。首先,引入一阶逻辑中的谓词追踪,建立系统内部功能需求与交互功能需求形式化规约方法。其次,针对单条、多条需求内容正确性以及需求关系一致性,构建需求一致性检查形式化规约,开展需求自冲突、集冲突与需求关系一致性检验,并生成可解释的检查反例进行需求迭代。最后,以机载平视显示(head-up display,HUD)系统飞行信息符号生成与显示功能为例,验证该方法的正确性与有效性。研究结果表明,基于有限谓词追踪的功能需求一致性检查方法能够提高需求一致性检查效率、降低研发成本,为民机系统级需求确认提供支持。
Requirement consistency checking method for civil aircraft systems based on finite predicate tracing
To address the problem that it is difficult to confirm the correctness of system-level requirements in the forward development process of safety-critical systems for civil aircraft,a functional requirement consistency checking system based on limited predicate tracking is proposed.Firstly,the predicate tracking in first-order logic is introduced to establish a formal statute method for internal and interactive functional requirements of sytem.Secondly,a formal statute for requirement consistency checking for single and multiple requirement content correctness and requirement relationship consistency are constructed.The requirement self-conflict,set conflict and requirement relationship consistency checking are carried out.And the interpretable check counterexamples for requirement iteration is generated.Finally,the correctness and effectiveness of the method are verified by taking the head-up display(HUD)system flight information symbol generation and display function as an example.The conclusion shows that the finite predicate tracking-based functional requirement consistency checking method can improve the efficiency of requirement consistency checking,reduce the development cost,and provide support for system-level requirement validation of civil aircraft.

requirements consistencytheorem provingcorrectness of functional requirementsfirst-order logic(FOL)requirements conflict

王鹏、岳舒婷、张帆、董磊

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中国民航大学民航航空器适航审定技术重点实验室,天津 300300

中国民航大学安全科学与工程学院,天津 300300

需求一致性 定理证明 功能需求正确性 一阶逻辑 需求冲突

中央高校基本科研业务费

3122022094

2024

系统工程与电子技术
中国航天科工防御技术研究院 中国宇航学会 中国系统工程学会

系统工程与电子技术

CSTPCD北大核心
影响因子:0.847
ISSN:1001-506X
年,卷(期):2024.46(1)
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