基于DoDAF的民机MBSE研制方法

doi:10.12305/j.issn.1001-506X.2021.12.20

Abstract

Abstract:

Aiming at a series of problems in the traditional civil aircraft development methods, such as incomplete design requirements, difficulty in ensuring the consistency of design and requirements, and difficulty in changing design schemes, to propose a U.S.Department of Defense Architecture Framework (DoDAF)-based civil aircraft model-based systems engineering(MBSE) development method is proposed which combines multiple perspectives of the DoDAF framework. This method refers to different viewpoints in DODAF to decompose and refine the requirements of civil aircraft development from multiple perspectives, generate resource flow models, activity models, and system interface models. And a more three-dimensional aircraft capability model is developed to guide the design of civil aircraft. It is proved that the DoDAF-based civil aircraft development method can completely and comprehensively decompose aircraft capability requirements from a multi-perspective and transform them into specific design requirements, so as to better guide the development of civil aircraft and improve the efficiency of civil aircraft development.

Key words: model-based systems engineering, the U.S.Department of Defense Architecture Framework (DoDAF), systems modeling language (SysML), civil aircraft

CLC Number:

Yunong WANG, Wenhao BI, An ZHANG, Chao ZHAN. DoDAF-based civil aircraft MBSE development method[J]. Systems Engineering and Electronics, 2021, 43(12): 3579-3585.

Figures/Tables 10

Fig.1

Fig.2

Table 1

Fig.3

Fig.4

Fig.5

Fig.6

Fig.7

Fig.8

Fig.9

References 28

1	李为吉. 飞机总体设计[M]. 西安: 西北工业大学出版社, 2005.
	LI W J . Aircraft configuration design[M]. Xi'an: Northwes-tern Polytechnical University Press, 2005.
2	张恩学, 余丽萍, 臧阳阳, 等. 如何发挥民机质量师系统在型号研制中的作用[J]. 航空标准化与质量, 2020, 299 (2): 33- 37.
	ZHANG E X , YU L P , ZANG Y Y , et al. How to play the role of civil aircraft quality engineer system in model development[J]. Aeronautic Standardization & Quality, 2020, 299 (2): 33- 37.
3	郭博志, 李浩敏. 大型客机设计中的需求管理[J]. 民用飞机设计与研究, 2013, (4): 1- 5. doi: 10.3969/j.issn.1674-9804.2013.04.001
	GUO B Z , LI H M . The application of requirements management in civil aircraft development[J]. Civil Aircraft Design and Research, 2013, (4): 1- 5. doi: 10.3969/j.issn.1674-9804.2013.04.001
4	IAN M , ALLAN S . Aircraft systems-mechanical, electrical and avionics subsystems integration[M]. NewYork: Wiley, 2008.
5	FRIEDENTHAL S, GRIEGO R, SAMPSON M. INCOSE model based systems engineering (MBSE) initiative[C]//Proc. of the INCOSE Symposium, 2007.
6	陈红涛, 邓昱晨, 袁建华, 等. 基于模型的系统工程的基本原理[J]. 中国航天, 2016, 32 (3): 18- 23.
	CHEN H T , DENG Y C , YUAN J H , et al. Fundamentals of model-based systems engineering[J]. Aerospace China, 2016, 32 (3): 18- 23.
7	STOEWER H , LIN C . Results from the panel on "MBSE transition towards the digital enterprise-where do we go from here?"[J]. Insight, 2019, 22 (1): 51- 53. doi: 10.1002/inst.12239
8	HULDT T , STENIUS I . State-of-practice survey of model-based systems engineering[J]. Systems Engineering, 2019, 22 (2): 134- 145. doi: 10.1002/sys.21466
9	KHOKHLOVSKIY V, OLEINIKOV V. Model-based systems engineering of process control for energy installations[C]//Proc. of the International Multi-Conference on Industrial Engineering and Modern Technologies, 2019.
10	DINGLE B M, EUBANKS J C, JANASAK K. 3D RAM modeling and simulation in a model based systems engineering environment[C]//Proc. of the Annual Reliability and Maintainability Symposium, 2020.
11	KAN Y B , ZHAO X Y , ACADEMY D N . Model-based system engineering method for outline design of maritime formation command and control system[J]. Computer & Digital Engineering, 2019, (9): 2201- 2205.
12	KASLOW D, ANDERSON L, ASUNDI S, et al. Developing a cubesat model-based system engineering reference model-interim status[C]//Proc. of the Aerospace Conference, 2015.
13	FERREIRA T , GORLACH I A . Development of an automated guided vehicle controller using a model-based systems engineering approach[J]. South African Journal of Industrial Engineering, 2016, 27 (2): 206- 217.
14	PESSA C, CIFALDI M, BRUSA E, et al. Integration of different MBSE approaches within the design of a control maintenance system applied to the aircraft fuel system[C]//Proc. of the IEEE International Symposium on Systems Engineering, 2016.
15	FUSARO R, FERRETTO D, VIOLA N. Model-based object-oriented systems engineering methodology for the conceptual design of a hypersonic transportation system[C]//Proc. of the IEEE International Symposium on Systems Engineering, 2016.
16	张贺, 魏强, 陈余军, 等. 基于SysML的通信卫星转发器系统设计[J]. 环境技术, 2019, 37 (2): 116- 122.
	ZHANG H , WEI Q , CHEN Y Q , et al. The design of communication satellite transponder system based on SysML[J]. Environmental Technology, 2019, 37 (2): 116- 122.
17	SCOTT D , SEAN B , TIM F , et al. Method for tracking and communicating aggregate risk through the use of model-based systems engineering (MBSE) tools[J]. Journal of Space Safety Engineering, 2020, 7 (1): 11- 17. doi: 10.1016/j.jsse.2020.01.001
18	PATOU F , DIMAKI M , MAIER A , et al. Model-based systems engineering for life-sciences instrumentation development[J]. Systems Engineering, 2019, 22 (2): 98- 113. doi: 10.1002/sys.21429
19	JOANNOU D , KALAWSKY R , SARAVI S , et al. A model-based engineering methodology and architecture for resilience in systems-of-systems: a case of water supply resilience to flooding[J]. Water, 2019, 11 (3): 496. doi: 10.3390/w11030496
20	KRUPA G P . Application of agile model-based systems engineering in aircraft conceptual design[J]. The Aeronautical Journal, 2019, 123 (1268): 1561- 1601. doi: 10.1017/aer.2019.53
21	LISCOUET H S, MOHAN B R, NELSON P J, et al. Evaluating a model-based systems engineering approach for the conceptual design of advanced aircraft high-lift system architectures[C]// Proc. of the Canadian Aeronautics and Space Institute AERO Confe-rence, 2017.
22	吴娟. 基于SysML的DoDAF产品设计研究[D]. 武汉: 华中科技大学, 2006.
	WU J. DoDAF product design based on SysML[D]. Wuhan: Huazhong University of Science and Technology, 2006.
23	KHARRAT M , PENAS O , PLATEAUX R , et al. Integration of electromagnetic constraints as of the conceptual design through an MBSE approach[J]. IEEE Systems Journal, 2020, 15 (1): 747- 758.
24	ZHOU X E , FANG Z M , SONG A . Architectural models enabled dynamic optimization for system of systems evolution[J]. Complexity, 2020, 7534819.
25	The Access 5 Project Systems Engineering & Integration Team. Hale UAS concept of operations[R]. Edwards: NASA UAV National Industry Team, 2006: 7-44.
26	HAUSE M . Integrating security into enterprise architecture with UAF and PLE[J]. Insight, 2020, 23 (3): 1- 30. doi: 10.1002/inst.12228
27	DOROFEEV A , ALTUKHOVA N , FILIPPOVA N , et al. Deve-lopment of transportation management system with the use of ontological and architectural approaches to ensure trucking reliability[J]. Sustainability, 2020, 12, 8504. doi: 10.3390/su12208504
28	陈宗基, 张平. 民机飞行控制系统设计的理论和方法[M]. 上海: 上海交通大学出版社, 2015.
	CHEN J Z , ZHANG P . The theory and method of civil aircraft flight control system design[M]. Shanghai: Shanghai Jiaotong University Press, 2015.

状态	能力愿景
起飞	根据飞行员输入的航路点制订飞行计划并根据航段信息计算燃料、时间消耗等。在跑道上加速至决断速度V₁, 控制机头上扬; 继续加速至抬轮速度V_R, 抬起前轮; 继续加速至安全起飞速度V₂, 离开跑道并收起起落架; 在引导下继续加速至爬升速度。
爬升	在最优爬升剖面内爬升至巡航高度, 分持续爬升和阶段性爬升两种。
巡航	飞机以最优巡航速度和最优巡航高度在最优巡航剖面内飞行。
下降	沿预计轨迹逐渐降低高度并减速。
进近	飞机在机场上空由地面管制人员指挥对准跑道下降的阶段。这个阶段飞机需要按规则绕机场飞行后直接对准跑道, 飞机减速, 放下襟翼和起落架。
着陆	当飞机下滑到离地面7~8 m高度时, 把机头拉起。到1 m左右高度时使飞机拉平, 飞机以平行地面姿态下降, 飞机两个主轮平衡着地, 飞机前轮仍然离地, 以一定迎角滑跑一段距离以增加阻力, 然后前推驾驶杆使前轮着地, 这时使用刹车, 和反推装置(喷气飞机)或反桨装置(螺旋桨飞机)使飞机尽快把速度减低, 滑出跑道, 进入滑行道, 驶向机坪。

[1]	Yaohua LI, Yuan GAO. Safety analysis for civil aircraft system based on STPA-ANP model [J]. Systems Engineering and Electronics, 2022, 44(9): 2986-2994.
[2]	Yunwen FENG, Junyu CHEN, Cheng LU. Research on civil aircraft spare parts multi-region support network model [J]. Systems Engineering and Electronics, 2022, 44(5): 1553-1561.
[3]	Yuanjie LU, Zhimin LIU, Zhixiao SUN, Dong KAN. Model-based integrated evaluation of UAV system architecture [J]. Systems Engineering and Electronics, 2022, 44(4): 1239-1245.
[4]	Qiucen FAN, Wenhao BI, An ZHANG, Wenhao WANG. MBSE modeling method of civil aircraft altitude control system [J]. Systems Engineering and Electronics, 2022, 44(1): 164-171.
[5]	Hongchen JIAO, Yong LEI, Hongyu ZHANG, Guobin ZHANG, Yaodong WANG. Research on modeling and design method of spacecraft system based on MBSE [J]. Systems Engineering and Electronics, 2021, 43(9): 2516-2525.
[6]	Delin LI, Wenhao BI, An ZHANG, Qiucen FAN. MBSE-based process management in the development of civil aircraft [J]. Systems Engineering and Electronics, 2021, 43(8): 2209-2220.
[7]	Wenhao WANG, Wenhao BI, An ZHANG, Qiucen FAN. Function modeling method of civil aircraft system based on MBSE [J]. Systems Engineering and Electronics, 2021, 43(10): 2884-2892.
[8]	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.
[9]	REN Bingxuan, LU Yi, FU Shan, HUANG Dan. Identification and verification of civil aircraft functional requirements through MBSE [J]. Systems Engineering and Electronics, 2019, 41(9): 2016-2024.
[10]	SUN Jian-zhong, ZUO Hong-fu. Bayesian method for system real-time performance reliability assessment [J]. Journal of Systems Engineering and Electronics, 2013, 35(8): 1790-1796.

DoDAF-based civil aircraft MBSE development method

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

Figures/Tables 10

References 28

Related Articles 10

Recommended Articles

Metrics

Comments