An algorithm design of sequential component in the aircraft electrical system

被引:0
|
作者
Zhao, Wenzhi [1 ]
机构
[1] Civil Aviat Univ China, Management Study Ctr, Tianjin, Peoples R China
关键词
sequential components; algorithm design; automatic calculation; over heat;
D O I
暂无
中图分类号
TP18 [人工智能理论];
学科分类号
081104 ; 0812 ; 0835 ; 1405 ;
摘要
An algorithm for the calculation of the sequential parameters in the aircraft electrical system is designed in this paper. The original calculation model of the sequential component calculation is given as a complex formula which is inconvenient for the general digital programmable computation. The geometrical algorithm is presented in this paper in which the voltage vectors rotate and project to the coordinate axis to simplify the calculation. The projections on x and y coordinates may add up in algebra way, and only one projection is left on each axis. Then synthesize the two components to obtain the required sequential voltage vector. This algorithm may be used in the program design by ordinary programming languages in the fault diagnostics and protection to the electrical system. The asymmetry calculation by hand is also made possible.
引用
收藏
页码:2413 / 2416
页数:4
相关论文
共 50 条
  • [1] Design and Verification of Aircraft Electrical Power System
    Sagirkaya, Huseyin
    [J]. 2023 IEEE INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE, ESARS-ITEC, 2023,
  • [2] Component Modeling and System Level Simulation of Aircraft Electrical Systems
    Li, Xiao
    Kher, Sameer
    Huang, Shimeng
    Ambalavanar, Vel
    Hu, Yang
    [J]. ENGINEERING LETTERS, 2016, 24 (02) : 178 - 186
  • [3] Design Algorithm of an Aircraft Power Generation System
    Ismagilov, Flur Rashitovich
    Kiselev, Mikhail Anatolyevich
    Vavilov, Viacheslav Evgenievich
    Gusakov, Denis Valerievich
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2019, 55 (06) : 2899 - 2910
  • [4] System Level Component Modeling of Aircraft Electrical System Using VHDL-AMS
    Li, Xiao
    Kher, Sameer
    Huang, Shimeng
    Ambalavanar, Vel
    Hu, Yang
    [J]. WORLD CONGRESS ON ENGINEERING AND COMPUTER SCIENCE, WCECS 2015, VOL II, 2015, : 841 - 846
  • [5] Design and Implementation of Simulation Maintenance Training System for Aircraft Engine Electrical System
    Wang, Zheng
    Zhu, Xingdong
    Fan, Jiali
    Song, Jianhua
    [J]. PROCEEDINGS OF THE 2ND INTERNATIONAL CONFERENCE ON ADVANCES IN MECHANICAL ENGINEERING AND INDUSTRIAL INFORMATICS (AMEII 2016), 2016, 73 : 1368 - 1373
  • [6] AIRCRAFT CARRIER ELECTRICAL-POWER SYSTEM-DESIGN PRACTICES
    SMITH, VB
    [J]. NAVAL ENGINEERS JOURNAL, 1977, 89 (04) : 83 - 91
  • [7] Load allocation problem for optimal design of aircraft electrical power system
    Giraud, X.
    Sartor, M.
    Roboam, X.
    Sareni, B.
    Piquet, H.
    Budinger, M.
    Vial, S.
    [J]. INTERNATIONAL JOURNAL OF APPLIED ELECTROMAGNETICS AND MECHANICS, 2013, 43 (1-2) : 37 - 49
  • [8] Parametric model of aircraft external geometry as a component of FAST-OAD aircraft preliminary design system
    Grendysa, Wojciech
    Jezegou, Joel
    Benard, Emmanuel
    [J]. 12TH EASN INTERNATIONAL CONFERENCE ON "INNOVATION IN AVIATION & SPACE FOR OPENING NEW HORIZONS", 2023, 2526
  • [9] Application of a negative selection algorithm to anomaly detection for aircraft electrical power system
    Dong, ES
    Dong, YG
    Jia, HC
    Li, J
    [J]. PROCEEDINGS OF THE THIRD INTERNATIONAL SYMPOSIUM ON INSTRUMENTATION SCIENCE AND TECHNOLOGY, VOL 3, 2004, : 1161 - 1164
  • [10] Research on Knowledge-based System for Typical Aircraft Composite Component Design
    Mei Zhongyi
    Zhu Sanshan
    Younus, Muhammad
    Saleem, Amir
    [J]. CEIS 2011, 2011, 15