基于UAF的月球探测工程设计与建模方法

李特; 胡震宇; 田少杰

doi:10.11728/cjss2025.05.2024-0127

基于UAF的月球探测工程设计与建模方法

doi: 10.11728/cjss2025.05.2024-0127 cstr: 32142.14.cjss.2024-0127

李特^1,,
胡震宇¹,
田少杰^{1, 2}

1.
深空探测实验室　北京　100195
2.
探月与航天工程中心　北京　100190

基金项目: 深空探测任务专项项目资助 (20221023)

详细信息

作者简介:

李特　男, 1987年5月出生于辽宁省本溪市, 现为深空探测实验室系统研究院工程师, 主要研究方向为深空探测工程总体技术研究、航天测控通信技术研究等. E-mail: dsel_lt@126.com

中图分类号: V57
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出版历程
- 收稿日期: 2024-10-12
- 修回日期: 2025-03-24
- 网络出版日期: 2025-03-25

Method of Design and Modeling for Lunar Exploration Engineering Based on UAF

LI Te^1
,,
HU Zhenyu¹,
TIAN Shaojie^{1, 2}

1.
Deep Space Exploration Laboratory, Beijing 100195
2.
Lunar exploration and Space Engineering Center, Beijing 100190

摘要

摘要: 针对月球探测工程中大系统设计与接口验证难点, 为有效解决需求、功能和接口等先期验证问题, 本文将统一体系结构框架 (UAF) 进行适应性裁剪和组合, 并结合系统工程方法论正向设计思想, 提出了基于UAF的月球探测工程设计与建模方法. 围绕月球探测任务全生命周期中关键环节, 构建了涵盖战略、业务、资源三个视点下相关领域的视图模型体系, 并以此为核心框架开展建模分析. 通过需求追溯和逻辑仿真迭代验证, 可辨识模型行为逻辑和接口匹配等问题, 指导模型完成优化改进, 提升了设计与建模的合理性和有效性. 研究结果可为月球探测工程顶层设计提供可行性参考.
- 月球探测工程 /
- 统一体系结构框架 /
- 设计与建模方法 /
- 视图模型
Abstract: Aiming at the difficulties in System Of System (SOS) design and interface verification in lunar exploration engineering, in order to effectively solve the pre-validation problems of requirements, functions and interfaces, under the conditions of adaptive tailoring and combination for Unified Architecture Framework (UAF), the method of design and modeling for lunar exploration engineering based on UAF is proposed, which is combined with the methodology of systems engineering on the forward design ideology. Focusing on the key links in full lifecycle of lunar exploration mission, the view model systems covered with strategic, operational and resource viewpoints of related fields are established, which are taken as the core framework to carry out modeling analysis. Through requirements traceability and logical simulation iterative validation, the models can be identified problems of behavioral logic and interface matching, and be guided to complete optimization and improvement, and also it improves the rationality and effectiveness of design and modeling. The results provide a feasible reference for the SOS design of lunar exploration engineering.
- Lunar exploration engineering /
- Unified Architecture Framework (UAF) /
- Method of design and modeling /
- View modeling

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图 1 基于UAF的正向设计与建模流程

Figure 1. Forward design and modeling process based on UAF

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图 2 战略流程

Figure 2. Strategic process view

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图 3 战略结构

Figure 3. Strategic structure view

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图 4 战略连通

Figure 4. Strategic connectivity view

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图 5 业务分类

Figure 5. Operational taxonomy view

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图 6 业务结构

Figure 6. Operational structure view

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图 7 业务流程

Figure 7. Operational process view

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图 8 业务序列

Figure 8. Operational sequence view

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图 9 业务状态

Figure 9. Operational state view

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图 10 资源分类

Figure 10. Resources taxonomy view

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图 11 资源结构

Figure 11. Resources structure view

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图 12 系统初始化资源流程

Figure 12. Resources process view of system initialization

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图 15 信息回传与分析资源流程

Figure 15. Resources process view of information transmission and analysis

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图 13 任务规划资源流程

Figure 13. Resources process view of mission planning

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图 14 任务执行资源流程

Figure 14. Resources process view of mission execution

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图 16 资源追溯

Figure 16. Resources traceability view

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图 17 资源流程模块定义

Figure 17. Block definition diagram of resources process view

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图 18 资源流程参数

Figure 18. Parametric diagram of resources process view

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图 19 资源流程图仿真分析

Figure 19. Simulation analysis of resources process view

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表 1 各阶段的视图定义

Table 1. View definition for each phase

阶段	视图	定义与描述
需求分析	战略流程(St-Pr)	为实现战略目标, 在任务全流程, 明确大系统应具备的顶层能力, 以及涉及的系统组织
	战略结构(St-Sr)	明确了顶层能力的组成、分解和层次结构
	战略连通(St-Cn)	明确了能力结构中相互依赖关系, 使能力分解合理化

功能分析	业务分类(Op-Tx)	描述了支持能力实现的具体业务活动, 建立业务活动与主要执行者间的操作关系
	业务结构(Op-Sr)	描述了业务各节点之间的连接和信息交互关系
	业务流程(Op-Pr)	基于行为, 描述了业务活动执行的过程、输入输出和信息流
	业务序列(Op-Sq)	基于场景对业务交换的时序进行分析和事件跟踪, 描述了关键事件的时序操作
	业务状态(Op-St)	基于状态转换的过程, 描述了业务的状态、事件和操作

架构分析	资源分类(Rs-Tx)	基于功能分析描述了资源的逻辑域解决方案

架构设计	资源结构(Rs-Sr)	描述了资源接口和交互关系
	资源流程(Rs-Pr)	基于行为分解, 在资源视点下描述了业务活动执行的过程、输入输出和信息流
	资源追溯(Rs-Tr)	描述了资源到业务活动、资源到能力的追溯关系

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表 2 关键活动参数设置

Table 2. Parameter settings of key action

关键活动	参数设置	备注
给各器上电	供电功率≥1500 W	太阳能、蓄电池
月面各器分离	释放重量≥200 kg	各器重量
器间通信	通信码速率≥1.2 kbit·s^–1	UHF通信体制

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