Application of Harmony SE in civil aircraft design

被引：0
|
作者：
Liu W. [1 ]
Feng Y. [1 ]
Hou J. [2 ]
Chen J. [1 ]
Guo Y. [1 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi'an
[2] Beijing Institute of Astronautical Systems Engineering, Beijing
来源：
Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University | 2024年 / 42卷 / 01期
关键词：
architecture model; civil aircraft; fuel tank pressurization component; Harmony SE; model-based system engineering (MBSE);
D O I：
10.1051/jnwpu/20244210035
中图分类号：
学科分类号：
摘要：
With the refinement of civil aircraft technology and the enhancement of product complexity, civil aircraft design has changed from traditional text-based system engineering to model-based system engineering, the expression of the system has also transformed from text-centered to model-centered. To further improve the model quality and correctness of aircraft system modeling, this paper explores the applicability of model-driven and verification-oriented system engineering methods in the field of civil aircraft design, and establishes the system engineering practice framework of civil aircraft design, which can ensure the rapid design and efficient delivery of civil aircraft. Firstly, starting from the Harmony SE modeling method, the workflow and modeling ideas of system are introduced; then the noticeable problems in the practice of civil aircraft system engineering are analyzed, and the system engineering practice of civil aircraft design is established with the support of the applicability of the Harmony SE method; finally, the fuel tank pressurization component is taken as the research object of the practice system in component-level. The results show that the system engineering practice framework of civil aircraft design and method proposed in this paper can correctly and reasonably allocate design requirements and establish a complete system model, which is helpful to improve the efficiency and accuracy of civil aircraft design at this stage. ©2024 Journal of Northwestern Polytechnical University.
引用
下载
收藏
页码：35 / 44
页数：9
相关论文
共 22 条
  • [1] WIBBEN DR, FURFARO R., Model-based systems engineering approach for the development of the science processing and operations center of the NASA OSIRIS-REx asteroid sample return mission, Acta Astronautica, 115, C, pp. 147-159, (2015)
  • [2] GOUGH K M, PHOJANAMONGKOLKIJ N., Employing model-based systems engineering(MBSE) on a NASA aeronautic research project: a case study, 2018 Aviation Technology, Integration, and Operations Conference, (2018)
  • [3] FAN Qiucen, BI Wenhao, ZHANG An, Et al., MBSE modeling method of civil aircraft altitude control system, Systems Engineering and Electronics, 44, 1, pp. 164-171, (2022)
  • [4] GREGORY J, BERTHOUD L, TRYFONAS T, Et al., The long and winding road: MBSE adoption for functional avionics of spacecraft, The Journal of Systems & Software, 160, (2020)
  • [5] WU Ying, LIU Juntang, ZHENG Dangdang, Research on the technology of method based system engineering, Aeronautical Science & Technology, 26, 9, pp. 69-73, (2015)
  • [6] ZHU Jing, YANG Hui, GAO Yahui, Et al., Summary of model based system engineering, Aeroengine, 42, 4, pp. 12-16, (2016)
  • [7] YAN Jie, Research on MBSE architecture modeling of civil aircraft navigation system, (2021)
  • [8] PENG Xinjia, MA Zhenkang, Radar system design method based on Arcadia/ Capella, Shipboard Electronic Countermeasure, 45, 5, pp. 21-26, (2022)
  • [9] CUI Zhanbo, JING Bo, JIAO Xiaoxuan, Et al., Application research of MBSE technology in PHM of flight control system, Foreign Electronic Measurement Technology, 41, 3, pp. 69-78, (2022)
  • [10] MADNI A M., Exploiting augmented intelligence in systems engineering and engineered systems, Insight, 23, 1, pp. 31-36, (2020)
123