Study on Key Technology of High and Low Temperature Test System for Flight Control Unit

被引:0
|
作者
Zhou Qiang [1 ]
Hong Binbin [1 ]
机构
[1] Beihang Univ, Beijing 100191, Peoples R China
关键词
high and low temperature test; signal switching; data distributor; data selector; testing time;
D O I
10.4028/www.scientific.net/AMM.538.402
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
According to the engineering requirements of multiple sets of Flight control unit in high and low temperature test, a new test system based on CPCI bus with a signal switching and distribution unit is designed to increase test efficiency. This test system can switch serial test under programming control for multiple sets of flight control unit in a certain temperature gradient, saving the time of temperature change and staying warm, eliminating a lot of tedious manual operations. Theoretical analysis and engineering practice has proved that this test system significantly reduces the testing time in high and low temperature test up to thirty hours (five sets of DUT), namely that relative time efficiency is up to 75.4% (five sets of DUT). It also has some other advantages such as saving hardware resources and flexible use.
引用
收藏
页码:402 / 407
页数:6
相关论文
共 50 条
  • [1] Research on Parallel Test Technology for Flight Control Component Comprehensive Test System
    Yu, Fu
    Du, JiaLu
    Zhou, Qiang
    2020 CHINESE AUTOMATION CONGRESS (CAC 2020), 2020, : 1304 - 1308
  • [2] Study of Key Technology for Automatic Test and Fault Diagnosis System
    Chen Jianhui
    Lian Guangyao
    Gao Fengqi
    Song Yingchen
    PROCEEDINGS OF THE SECOND INTERNATIONAL SYMPOSIUM ON TEST AUTOMATION & INSTRUMENTATION, VOL. 3, 2008, : 1650 - 1653
  • [3] A Study on UAV Flight Control System HILS Test Environment
    Byun, Jinku
    Hur, Gi-Bong
    Lee, KwangHyun
    Suk, Jinyoung
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2016, 44 (04) : 316 - 323
  • [4] Automatic test system for flight control system
    Wu, H
    Guo, DG
    Wang, RC
    Yan, PX
    ISTM/2003: 5TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-6, CONFERENCE PROCEEDINGS, 2003, : 987 - 989
  • [5] Study on the Flight Test Risk Assessment of Civil Aircraft Flight Control System Failure
    Yang, Shi Bin
    Zhang, Jing
    Qin, Xian Xue
    Ma, Li Qun
    Yang, Jian Zhong
    JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION, 2020, 52 (02): : 171 - 181
  • [6] An Indigenous Flight Control System Test
    Akdeniz Agdere, Sadiye
    Karasubasi, Melih
    Sagirkaya, Huseyin
    2022 IEEE AUTOTESTCON, 2022,
  • [7] The Key Technology And Simulation Of UAV Flight Monitoring System
    Xue Pengbo
    Jin Guodong
    Lu Libin
    Tan Lining
    Ning Jigan
    PROCEEDINGS OF 2016 IEEE ADVANCED INFORMATION MANAGEMENT, COMMUNICATES, ELECTRONIC AND AUTOMATION CONTROL CONFERENCE (IMCEC 2016), 2016, : 1551 - 1557
  • [8] Study on the Key Technology of Integrated Analog Chip Test and System Design
    Liu Jingmeng
    Liao Min
    Chen Weihai
    Xu Dong
    ICIEA: 2009 4TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, VOLS 1-6, 2009, : 484 - +
  • [9] Study on key technology of control system for propeller processing machines
    Zhu, Guoli
    Gong, Shihua
    Li, Bin
    Huazhong Keji Daxue Xuebao (Ziran Kexue Ban)/Journal of Huazhong University of Science and Technology (Natural Science Edition), 2007, 35 (03): : 77 - 79
  • [10] STUDY OF THE BIT KEY TECHNOLOGY IN THE AIRBORNE MEASUREMENT AND CONTROL SYSTEM
    Fan, LiMing
    Wu, Peng
    Zhang, XiaoLin
    RECENT TRENDS IN MATERIALS AND MECHANICAL ENGINEERING MATERIALS, MECHATRONICS AND AUTOMATION, PTS 1-3, 2011, 55-57 : 1172 - 1176