基于MBSE的运载火箭上升段逃逸救生策略

doi:10.12305/j.issn.1001-506X.2023.04.20

系统工程与电子技术 ›› 2023, Vol. 45 ›› Issue (4): 1121-1126.doi: 10.12305/j.issn.1001-506X.2023.04.20

• 系统工程 • 上一篇

基于MBSE的运载火箭上升段逃逸救生策略

武新峰¹, 彭祺擘¹^,*, 黄冉¹, 李静琳²

1. 中国航天员科研训练中心, 北京 100094
2. 北京宇航系统工程研究所, 北京 073000

收稿日期:2022-03-23 出版日期:2023-03-29 发布日期:2023-03-28
通讯作者: 彭祺擘
作者简介:武新峰 (1983—), 男, 助理研究员, 博士, 主要研究方向为载人登月总体任务分析、飞行器设计
彭祺擘 (1982—), 男, 副研究员, 博士, 主要研究方向为载人登月总体任务分析与设计
黄冉 (1982—), 女, 副研究员, 硕士, 主要研究方向为载人登月总体方案论证、载人航天数字化总体设计
李静琳 (1991—), 女, 工程师, 博士, 主要研究方向为运载火箭弹道制导设计

Escape and rescue strategy of launch vehicle ascending section based on MBSE

Xinfeng WU¹, Qibo PENG¹^,*, Ran HUANG¹, Jinglin LI²

1. China Astronaut Research and Training Center, Beijing 100094, China
2. Beijing Institute of Astronautical Systems Engineering, Beijing 073000, China

Received:2022-03-23 Online:2023-03-29 Published:2023-03-28
Contact: Qibo PENG

摘要/Abstract

摘要：

为提高运载火箭上升段逃逸救生策略的覆盖性和有效性，采用基于模型的系统工程(model-based system engineering, MBSE)方法开展设计。首先, 进行运载火箭逃逸救生任务分析, 识别相关系统及其任务需求, 建立任务需求模型。然后, 根据运载火箭飞行程序, 建立不同时刻的主要故障模型, 研究提出不同故障的可能应对策略, 形成功能需求模型。最后, 在逻辑仿真中调用弹道仿真程序, 验证了逃逸救生策略的可行性, 实现了需求的闭环验证。通过采用该方法, 完成了运载火箭上升段逃逸救生任务需求模型化, 奠定了全任务周期数字化设计的基础, 可为工程实践提供参考。

关键词: 运载火箭, 载人飞船, 逃逸救生, 基于模型的系统工程方法

Abstract:

In order to improve the coverage and effectiveness of the escape and rescue strategy of launch vehicle ascending section, the model-based system engineering(MBSE) method is used in the scheme design. Firstly, the mission analysis of escape and rescue for the new launch vehicle is carried out to identify the related systems and their mission requirements, and then the requirement model is established. Then, according to the launch vehicle flight procedures, the main fault models at different time are established, and the possible coping strategies for different faults are studied and proposed to form the functional requirements model.Finally, the trajectory simulation program is called in the logic simulation to verify the feasibility of escape and rescue strategies, and then the closed-loop verification of the requirements is realized. By adopting this method, the requirement modeling of the escape and rescue mission of launch vehicles ascending section is completed, and the foundation of digital design of full mission cycle is laid, which can provide reference for engineering practice.

Key words: launch vehicle, manned spacecraft, escape and rescue, model-based system engineering (MBSE) method

中图分类号:

武新峰, 彭祺擘, 黄冉, 李静琳. 基于MBSE的运载火箭上升段逃逸救生策略[J]. 系统工程与电子技术, 2023, 45(4): 1121-1126.

Xinfeng WU, Qibo PENG, Ran HUANG, Jinglin LI. Escape and rescue strategy of launch vehicle ascending section based on MBSE[J]. Systems Engineering and Electronics, 2023, 45(4): 1121-1126.

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参考文献 29

1	郭宝柱. 中国航天系统工程方法与实践[J]. 复杂系统与复杂性科学, 2004, 1 (2): 16- 19.
	GUO B Z . China aerospace systems engineering methods and practices[J]. Complex Systems and Complexity Science, 2004, 1 (2): 16- 19.
2	NA SA . Expanded guidance for NASA systems engineering: crosscutting topics, special topics, and appendices[M]. Washington D. C.: NASA Headquarters, 2016: 94- 110.
3	FRIEDENTHAL S , ALAN M , RICK S . A practical guide to SysML: the systems modeling language[M]. Amsterdam: Elsevier, 2015.
4	MANN C . A practical guide to SysML: the systems modeling language[J]. Kybernetes, 2009, 38 (2): 989- 994.
5	FORTESCUE P , SWINERD G , STARK J . Spacecraft systems engineering[M]. 4th ed West Sussex: Wiley, 2014: 168- 179.
6	YILDIRIM U , CAMPEAN F , WILLIAMS H . Function modeling using the system state flow diagram[J]. Artificial Intelligence for Engineering Design Analysis and Manufacturing, 2017, 31 (4): 413- 435. doi: 10.1017/S0890060417000294
7	李明华. 航天复杂巨系统工程管理体系及实施初探[J]. 工程研究, 2020, 12 (2): 155- 163.
	LI M H . Preliminary exploration of engineering management system of complex giant aerospace system and implementation[J]. Journal of Engineering Studies, 2020, 12 (2): 155- 163.
8	LEMAZURIER L , CHAPURLAT V , GROSSETETE A . An MBSE approach to pass from requirements to functional architecture[J]. IFAC-Papers on Line, 2017, 50 (1): 7260- 7265. doi: 10.1016/j.ifacol.2017.08.1376
9	BERGMAN S, FRENCH M, KUHN F. System architecture studies for the energy optimized aircraft[C]//Proc. of the 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2013.
10	范秋岑, 毕文豪, 张安. 民用飞机高度控制系统MBSE建模方法[J]. 系统工程与电子技术, 2022, 44 (1): 164- 171.
	FAN Q C , BI W H , ZHANG A . MBSE modeling method of civil aircraft altitude control system[J]. Systems Engineering and Electronics, 2022, 44 (1): 164- 171.
11	JIA Z R , LU F X , WANG H Y . Multi-stage attack weapon target allocation method based on defense area analysis[J]. Journal of Systems Engineering and Electronics, 2020, 31 (3): 539- 550. doi: 10.23919/JSEE.2020.000033
12	刘继忠, 裴照宇, 于国斌. 航天工程多态全息模型及应用[J]. 宇航学报, 2019, 40 (5): 535- 542.
	LIU J Z , PEI Z Y , YU G B . Space engineering multi-state holographic model and its applications[J]. Journal of Astronaut, 2019, 40 (5): 535- 542.
13	XIAO F, CHEN B, LI R, et al. A model-based system engineering approach for aviation system design by applying Sysml modeling[C]//Proc. of the Chinese Control and Decision Conference, 2020.
14	WANG H L , ZHONG D M , ZHAO T D , et al. Integrating model checking with SysML in complex system safety analysis[J]. IEEE Access, 2019, 7, 16561- 16571. doi: 10.1109/ACCESS.2019.2892745
15	焦洪臣, 雷勇, 张宏宇. 基于MBSE的航天器系统建模分析与设计研制方法探索[J]. 系统工程与电子技术, 2021, 43 (9): 2516- 2525.
	JIAO H C , LEI Y , ZHANG H Y . Research on modeling and design method of spacecraft system based on MBSE[J]. Systems Engineering and Electronics, 2021, 43 (9): 2516- 2525.
16	HOFFMANN H. SysML-based systems engineering using a model-driven development approach[C]//Proc. of the INCOSE International Symposium, 2006, 16(1): 804-814.
17	KASLOW D, AYRES B J, CAHILL P T, et al. CubeSat model-based system engineering (MBSE) reference model-development and distribution-interim status[C]//Proc. of the Small Satellite Conference, 2016.
18	CENCETTI M, PASQUINELLI M, MAGGIORE P. System modeling framework and MDO tool integration: MBSE methodologies applied to design and analysis of space system[C]//Proc. of the AIAA Modeling and Simulation Technologies Conference, 2013.
19	WANG H Q, ZHANGT J, JIANG B C. An integrated analysis and modeling framework for weapon equipment system evolution[C]//Proc. of the 6th International Symposium on Project Management, 2018.
20	FRIEDENTHAL S , ALAN M , RICK S . A practical guide to SysML: the systems modeling language[M]. Amsterdam: Elsevier, 2015.
21	张兵, 沈丹, 张志国. 长征系列运载火箭飞行智能化发展路线研究[J]. 导弹与航天运载技术, 2021, (1): 7- 11.
	ZHANG B , SHEN D , ZHANG Z G . The intelligent flight roadmap of long march launch vehicle[J]. Missiles and Space Vehicles, 2021, (1): 7- 11.
22	鲁宇. 中国运载火箭技术发展[J]. 宇航总体技术, 2017, 1 (3): 1- 8.
	LU Y . Space launch vehicle's development in china[J]. Astronautical Systems Engineering Technology, 2017, 1 (3): 1- 8.
23	谭述君, 何骁, 张立勇. 运载火箭推力故障下基于智能决策的在线轨迹重规划方法[J]. 宇航学报, 2021, 42 (10): 1228- 1236.
	TAN S J , HE X , ZHANG L Y . Online trajectory replanning method based on intelligent decision-making for launch vehicles under thrust drop failure[J]. Journal of Astronautics, 2021, 42 (10): 1228- 1236.
24	张荣升, 吴燕生, 秦旭东. 运载火箭推力下降故障下的在线弹道重构方法[J]. 南京航空航天大学学报, 2021, 53 (S1): 25- 31.
	ZHANG R S , WU Y S , QIN X D . Online trajectory reconstruction of launch vehicle with thrust drop faults[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2021, 53 (S1): 25- 31.
25	李师尧, 常武权, 闫宇申. 运载火箭动力故障下的自主救援轨道规划[J]. 飞行力学, 2021, 39 (2): 83- 89.
	LI S Y , CHANG W Q , YUN Y S . Autonomous rescue orbit strategy for propulsion system failure of launch vehicle[J]. Flight Dynamics, 2021, 39 (2): 83- 89.
26	张智, 容易, 郑立伟, 等. 运载火箭动力冗余技术[J]. 载人航天, 2013, 19 (6): 15- 19.
	ZHANG Z , RONG Y , ZHENG L W , et al. Redundant propulsion technology for launch vehicle[J]. Manned Spaceflight, 2013, 19 (6): 15- 19.
27	容易, 郑立伟, 常武权. 不同逃逸模式对运载火箭的影响研究[J]. 载人航天, 2018, 24 (3): 394- 399.
	RONG Y , ZHENG L W , CHANG W Q . Effects of various escape schemes on manned launch vehicles[J]. Manned Spaceflight, 2018, 24 (3): 394- 399.
28	常武权, 张志国. 运载火箭故障模式及制导自适应技术应用分析[J]. 宇航学报, 2019, 40 (3): 302- 309.
	CHANG W Q , ZHANG Z G . Analysis of fault modes and applications of self-adaptive guidance technology for launch vehicle[J]. Journal of Astronautics, 2019, 40 (3): 302- 309.
29	WANG X J. Development and prospect of launch vehicle technology for space station[C]//Proc. of the International Symposium on Outlook and Cooporation on Near-Earth Orbit Human Space Flight, 2022.

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基于MBSE的运载火箭上升段逃逸救生策略

Escape and rescue strategy of launch vehicle ascending section based on MBSE

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