|本期目录/Table of Contents|

[1]刘 远,杨恒辉,葛洋洋.基于实时操作系统的电子控制器仿真验证环境设计[J].工业仪表与自动化装置,2022,(02):121-125.[doi:10.19950/j.cnki.cn61-1121/th.2022.02.025]
 LIU Yuan,YANG Henghui,GE Yangyang.Research design of electronic controller simulation verification environment based on real-time operating system[J].Industrial Instrumentation & Automation,2022,(02):121-125.[doi:10.19950/j.cnki.cn61-1121/th.2022.02.025]
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基于实时操作系统的电子控制器仿真验证环境设计

《工业仪表与自动化装置》[ISSN:1000-0682/CN:61-1121/TH]

卷:
期数:
2022年02期
页码:
121-125
栏目:
出版日期:
2022-04-15

文章信息/Info

Title:
Research design of electronic controller simulation verification environment based on real-time operating system
文章编号:
1000-0682(2022)02-0000-00
作者:
刘 远杨恒辉葛洋洋
(航空工业西安航空计算技术研究所,陕西 西安 710076)
Author(s):
LIU YuanYANG HenghuiGE Yangyang
(AVIC Xi’an Aeronautics Computing Technique Research Institute,Shaanxi Xi’an 71006,China)
关键词:
电子控制器硬件在环实时仿真LabView
Keywords:
electronic controller hardware in the loop real-time simulation Labview
分类号:
TP273
DOI:
10.19950/j.cnki.cn61-1121/th.2022.02.025
文献标志码:
A
摘要:
航空发动机作为整个飞机中的核心部件,发生任何故障都会对飞机造成严重的威胁,电子控制器作为发动机系统的中枢指挥,承担着发动机控制、紧急情况响应等关键任务。为保证航发控制器能可靠高效地工作,必须要对其进行全方位、多角度、广范围的迭代验证。硬件在环仿真平台够进行电子控制器全状态功能与性能的仿真模拟,能够有效节约成本、缩短研发周期、降低试车风险,已成为发动机控制器研制过程中的关键技术之一。该文研制了一套仿真验证平台,该平台借助LabView与VeriStand软件,配合各类板卡能实现涡轴发动机控制系统的实时仿真、可对电子控制器进行全功能、性能的仿真验证,为电子控制器的研制提供了有力可靠的支撑。
Abstract:
Aero-engine is the core component of the whole aircraft, and any failure will pose a serious threat to the aircraft. As the central command of the engine system, the electronic controller undertakes the key tasks such as engine control and emergency response. In order to ensure the reliable and efficient operation of the air engine controller, it is necessary to carry out all-round, multi-angle and wide range iteration verification. The hardware in the loop simulation platform can be used to simulate the full state functions and performance of the electronic controller, which can effectively save the cost, shorten the development cycle and reduce the risk of test run. It has become one of the key technologies in the development process of the engine controller. This paper developed a set of simulation verification platform. The platform consists of LabView, VeriStand, and various kinds of board cards, which can realize the real-time simulation of the control system of the turboshaft engine. The electronic controller can carry out full function, performance simulation verification, for the development of the electronic controller provides a strong and reliable support.

参考文献/References:

[1]赵小勇,赵刚,杨恒辉.小型涡轴发动机数控系统硬件在回路仿真技术研究[J].测控技术,2012,31(07):46-49.

[2]蔡开龙,谢寿生,胡金海,等.涡扇发动机燃油综合控制半实物仿真试验系统[J].推进技术,2007(4):422-427.
[3]杨东升,王高峰.多线程技术在虚拟仪器开发软件LabWindows/CVI中的实现[J].电测与仪表,2005(3):39-41+54.
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相似文献/References:

[1]言洁奕,李 伟,王城麟,等.电气装置适应航空发动机电源故障试验的优化设计[J].工业仪表与自动化装置,2017,(06):56.[doi:1000-0682(2017)06-0056-04]
 YAN Jieyi,LI Wei,WANG Chenglin,et al.Optimal design of electric device to adapt to aeroengine power failure test[J].Industrial Instrumentation & Automation,2017,(02):56.[doi:1000-0682(2017)06-0056-04]

备注/Memo

备注/Memo:
收稿日期:2021-12-20

作者简介:
刘远(1994),男,硕士,助理工程师,辅助动力装置控制系统。
更新日期/Last Update: 1900-01-01