基于需求-功能-结构关系矩阵的导弹模块划分方法

doi:10.12305/j.issn.1001-506X.2024.10.17

摘要/Abstract

摘要：

模块化导弹能够利用分系统的灵活装配快速形成典型作战单元以适应复杂多样化的作战任务, 是未来导弹武器系统的重要发展方向之一。针对传统的导弹模块划分方法无法充分发挥导弹模块化特性带来的架构优势问题, 提出一种基于需求-功能-结构关系矩阵的导弹模块划分方法。首先, 基于质量功能展开(quality function deployment, QFD)和公理设计方法提出连接设计需求、设计功能与物理组件相互作用关系的设计结构矩阵(design structure matrix, DSM)构建方法, 并引入约束矩阵描述物理组件在机械、电气和功能上的关联度, 以此形成基于遗传算法的导弹模块划分流程。最后, 以一防空导弹为应用实例进行模块划分, 并通过需求回溯分析验证模块划分结果的合理性和可行性。

关键词: 模块划分, 模块化导弹, 设计结构矩阵, 需求分析, 公理设计, 质量屋

Abstract:

Modular missile can make use of the flexible assembly of subsystems to quickly form a typical combat unit to adapt to complex and diversified combat tasks, which is one of the important development directions of future missile weapon systems. Aiming at the problem that the traditional missile module division method can not give full play to the architectural advantages brought by the modular characteristics of missiles, a missile module division method based on demand-function-structure relationship matrix is proposed. Firstly, based on quality function deployment (QFD) and axiomatic design methods, a design structure matrix (DSM) construction method is proposed to connect the interaction relationship between the design requirements, design functions and physical components. Constraint matrix is introduced to describe the correlation degree of physical components in mechanical, electrical and functional aspects, so as to form a missile module division process based on genetic algorithm. Finally, an air defense missile is used as an application example for module division, and the rationality and feasibility of the module division results are verified through requirement backtracking analysis.

Key words: module division, modular missile, design structure matrix, demand analysis, axiomatic design, house of quality

中图分类号:

田昆效, 粟华, 龙永松, 杨予成, 龚春林. 基于需求-功能-结构关系矩阵的导弹模块划分方法[J]. 系统工程与电子技术, 2024, 46(10): 3398-3406.

Kunxiao TIAN, Hua SU, Yongsong LONG, Yucheng YANG, Chunlin GONG. Module division method of missile based on requirement-function-structure relation matrix[J]. Systems Engineering and Electronics, 2024, 46(10): 3398-3406.

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评估值r	相关性描述
0	需求要素与设计功能无关
1	需求要素与设计功能的相关性较小
3	需求要素与设计功能的相关性较大
5	需求要素与设计功能的相关性很大

关联度a	机械相关性描述
0	没有机械接口
[0.25~0.5]	能拆卸的固定接口, 无特殊形位公差设计
(0.5~0.75]	能拆卸的固定接口, 有形位公差设计
(0.75~1]	固定连接才能完成特定功能, 有较高形位公差设计需求

关联度b	电气相关性描述
0	无标准机械接口, 不存在信息传递
[0.3~0.5]	无标准机械接口, 存在信息传递
(0.5~0.7]	有标准机械接口, 存在信息传递
(0.7~1]	有标准机械接口, 存在信息传递或需进行固定连接才能实现特定功能

关联度c	功能相关性描述
0	设计功能独立
[0.25~0.4]	少部分设计功能相同
(0.4~0.6]	部分设计功能相同
(0.6~1]	设计功能基本相同

编号	组件名称	编号	组件名称
1	复合战斗部	10	走线仓
2	电子安执	11	发动机
3	安全执行机构	12	导航处理系统
4	复合导引头	13	舵翼
5	信息处理器	14	数据链系统
6	飞行控制处理器	15	壳体
7	电源	16	燃气舵
8	电气控制模块	17	弹翼
9	惯性测量设备	-	-