A Forward Development Method for Functional Design of Civil Aircraft Flight Control System

被引:0
|
作者
Cheng S. [1 ]
Li C. [2 ]
Zhang Y. [1 ]
Tang C. [2 ]
Meng X. [1 ]
Xie Y. [1 ]
机构
[1] School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai
[2] COMAC Shanghai Aircraft Design and Research Institute, Shanghai
关键词
flight control system; functional design; functional model; functional requirement;
D O I
10.16183/j.cnki.jsjtu.2022.100
中图分类号
学科分类号
摘要
Functional design is an extremely important part in the design and development of complex systems. It is necessary to establish a forward development method to ensure the correctness and completeness of functional design. Therefore,taking the flight control system of civil aircraft as an example,a forward development method for functional design is proposed. First, system modeling language is used to establish the functional requirements relationship model from aircraft level to system level and then to item level. Then,the functional requirements are combined with the safety requirements in SAE ARP4754A aircraft development guide to construct the functional knowledge set of the flight control system. Finally,the functional model of the flight control system is established based on functional unit block diagram and functional integration block diagram. This method can be used as a reference for the functional design of complex systems. © 2023 Shanghai Jiao Tong University. All rights reserved.
引用
收藏
页码:1305 / 1315
页数:10
相关论文
共 21 条
  • [1] GAO Jinyuan, FENG Huanan, Flight control system for civil aircraft, (2018)
  • [2] XIE Youbai, Thinking about MBSE and MBD, Science & Technology Review, 37, 7, pp. 6-11, (2019)
  • [3] KURTOGLU T, TUMER I Y., A graph-based fault identification and propagation framework for functional design of complex systems, Journal of Mechanical Design, 130, 5, (2008)
  • [4] NASYROV R, YUSUPOVA N, ZULKARNEEV R, Et al., The concept of decision support in evaluating the functional state of complex system of the biological type, Proceedings of the 21st International Workshop on Computer Science and Information Technologies, pp. 151-156, (2019)
  • [5] MADNI A M., MBSE testbed for rapid, cost-effective prototyping and evaluation of system modeling approaches, Applied Sciences, 11, 5, (2021)
  • [6] MEI Qian, HUANG Dan, LU Yi, Design method of civil aircraft functional architecture based on MBSE [J], Journal of Beijing University of Aeronautics & Astronautics, 45, 5, pp. 1042-1051, (2019)
  • [7] REN Bingxuan, LU Yi, FU Shan, Et al., Identification and verification of civil aircraft functional requirements through MBSE [J], Systems Engineering & Electronics, 41, 9, pp. 2016-2024, (2019)
  • [8] WANG Hao, GAO Yakui, SHU Yonging, Et al., Research on safety design technology of flight control system based on function model [J], Measurement & Control Technology, 36, 5, pp. 77-81, (2017)
  • [9] LAUKOTKA F, HANNA M, KRAUSE D., Digital twins of product families in aviation based on an MBSE-assisted approach, Procedia CIRP, 100, pp. 684-689, (2021)
  • [10] WANG Wenhao, BI Wenhao, ZHANG An, Et al., Function modeling method of civil aircraft system based on MBSE, Systems Engineering & Electronics, 43, 10, pp. 1-9, (2021)