System interface design of civil aircraft based on system engineering and the control method research

doi:10.11996/JG.j.2095-302X.2024020383

Abstract

Abstract:

The interface of civil aircraft systems should meet the requirements of functionality, performance and physical space. The design and control of system interfaces is one of the most important tasks in the design of civil aircraft airborne systems, subsystems, and equipment. Based on the concept of system engineering, taking the relevant requirements of interface definition and design of airborne system, subsystem and equipment as input, combined with the definition of airborne system development stage, this study proposes a hierarchical interface definition and design method based on interface design requirements, and a control strategy for interfaces at the same level and between the upper and lower levels. Combined with a civil atmospheric data subsystem, this study took the design and control of electrical interfaces as a typical case, and introduced the specific practices of interface design and control, thereby providing a practical reference for the design and control of various interfaces of civil aircraft airborne systems, subsystems, and equipment.

Key words: civil aircraft, airborne systems, system engineering, interface design, requirement

CLC Number:

V241

ZHANG Zhao, TANG Jian, WANG Hao, WANG Shiyuan. System interface design of civil aircraft based on system engineering and the control method research[J]. Journal of Graphics, 2024, 45(2): 383-387.

Figures/Tables 3

References 15

[1]	武瑞欢. 基于HKS289BRM的1553B总线通信接口设计[J]. 电脑编程技巧与维护, 2023(8): 166-169.
	WU R H. Design of 1553B bus communication interface based on HKS289BRM[J]. Computer Programming Skills & Maintenance, 2023(8): 166-169 (in Chinese).
[2]	张小红. 基于ZYNQ-7000的1553B总线接口设计[J]. 现代导航, 2021, 12(4): 276-279, 288.
	ZHANG X H. Design of 1553B bus interface based on zynq-7000[J]. Modern Navigation, 2021, 12(4): 276-279, 288 (in Chinese).
[3]	王越涛, 赵冬青, 武慧军. 基于FPGA和B61580S3的1553B总线RT/MT功能的设计与验证[J]. 电子设计工程, 2023, 31(2): 179-183.
	WANG Y T, ZHAO D Q, WU H J. Design and verification of 1553B bus RT/MT function based on FPGA and B61580S3[J]. Electronic Design Engineering, 2023, 31(2): 179-183 (in Chinese).
[4]	尹嘉乐, 彭良福. 基于国产FPGA的ARINC429总线接口的设计[J]. 电脑与信息技术, 2024, 32 (1): 82-85.
	YIN J L, PENG L F. Design of ARINC429 bus interface based on domestic FPGA[J]. Computer and Information Technology, 2024, 32(1): 82-85 (in Chinese).
[5]	孙骜, 秦旭军. 基于FPGA的多通道ARINC429总线测试系统[J]. 电子技术应用, 2023, 49(1): 119-123.
	SUN A, QIN X J. Multichannel ARINC429 bus test system based on FPGA[J]. Application of Electronic Technique, 2023, 49(1): 119-123 (in Chinese).
[6]	潘硕, 徐婕, 任杰, 等. ARINC429航空总线典型器件与接口设计[J]. 电子制作, 2023, 31(12): 82-84, 92.
	PAN S, XU J, REN J, et al. Typical devices and interface design of ARINC429 aviation bus[J]. Practical Electronics, 2023, 31(12): 82-84, 92 (in Chinese).
[7]	吕亚方, 米耘锋, 滕飞, 等. 基于HI3210的ARINC429总线标准接口设计与实现[J]. 信息通信, 2019, 32(2): 166-167.
	LV Y F, MI Y F, TENG F, et al. Design and implementation of ARINC429 bus standard interface based on HI3210[J]. Information & Communications, 2019, 32(2): 166-167 (in Chinese).
[8]	张文静. 民用飞机座舱显示与控制系统接口设计[J]. 中国高新技术企业, 2016(13): 18-20.
	ZHANG W J. Interface design of display and control system in civil aircraft cockpit[J]. China High-Tech Enterprises, 2016(13): 18-20 (in Chinese).
[9]	刘兆洋. 航电网络通用通信接口设计与实现[D]. 成都: 电子科技大学, 2018.
	LIU Z Y. Design and implementation of general communication interface in avionics network[D]. Chengdu: University of Electronic Science and Technology of China, 2018 (in Chinese).
[10]	朱岩, 王厉哲. 民用飞机动力装置系统机械接口设计研究[J]. 民用飞机设计与研究, 2016(4): 67-70.
	ZHU Y, WANG L Z. Study of mechanical interface design of powerplant system for civil aircraft[J]. Civil Aircraft Design & Research, 2016(4): 67-70 (in Chinese).
[11]	张琛. 民用飞机大气数据和惯性基准系统接口定义简介[J]. 科技资讯, 2015, 13(19): 22-23.
	ZHANG C. Brief introduction of interface definition of civil aircraft atmospheric data and inertial reference system[J]. Science & Technology Information, 2015, 13(19): 22-23 (in Chinese).
[12]	王坤宇, 武建文, 陈儒盎, 等. 航空电气系统接口电路设计与仿真研究[J]. 电器与能效管理技术, 2023, (8): 33-40.
	WANG K Y, WU J W, CHEN R A, et al. Study on design and simulation of aviation electrical system’s interface circuit[J]. Electrical & Energy Management Technology, 2023, (8): 33-40 (in Chinese).
[13]	张旭洲, 车炯晖, 李林. 一种航空机电系统通用输出接口设计方案[J]. 电脑知识与技术, 2019, 15(10): 202-203.
	ZHANG X Z, CHE J H, LI L. Design of a normalization interface for discrete and analog ouput on aircraft utility system[J]. Computer Knowledge and Technology, 2019, 15(10): 202-203 (in Chinese).
[14]	李竹, 杨凡. 民用飞机航电接口正向设计方法研究[J]. 民用飞机设计与研究, 2023(3): 70-75.
	LI Z, YANG F. Research on forward design method for civil aircraft avionics interface[J]. Civil Aircraft Design & Research, 2023(3): 70-75 (in Chinese).
[15]	白洁, 吕伟, 张磊, 等. 基于模型的系统工程在机载电子系统领域的应用[J]. 航空制造技术, 2015, 58(4): 96-99.
	BAI J, LV W, ZHANG L, et al. Application of model-based system engineering in area of airborne avionics system[J]. Aeronautical Manufacturing Technology, 2015, 58(4): 96-99 (in Chinese).

信号编号	信号名称	连接器(从-到)	针孔号 (从-到)	端接尺寸/ mm	屏蔽类型	导线线型	额定电压/ VDC	额定电流/ A	额定功率/ VA
N28063-1	AOA L1 Resolver 1	3U-275A- 3U-271B	3-1	22	360°	三扭绞屏蔽线	28	0.179	5
N28063-2	AOA L2 Resolver 1	3U-275A- 3U-271B	1-2	22	360°	三扭绞屏蔽线	28	0.179	5

信号编号	信号名称	连接器(从-到)	针孔号 (从-到)	端接尺寸/ mm	屏蔽类型	导线线型	额定电压/ VDC	额定电流/ A	额定功率/ VA
N28063-1	AOA L1 Resolver 1	3U-275A- 3U-271B	3-1	22	360°	三扭绞屏蔽线	28	0.179	5
N28063-2	AOA L2 Resolver 1	3U-275A- 3U-271B	1-2	22	360°	三扭绞屏蔽线	28	0.179	5