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飞机电传操纵及模拟加载系统实验台开发
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  • 英文篇名:Development of experimental platform for airplane fly-by-wire and electric loading system
  • 作者:孟忱 ; 郝魁红 ; 何永勃
  • 英文作者:Meng Chen;Hao Kuihong;He Yongbo;School of Aviation Automation,Civil Aviation University of China;
  • 关键词:飞机电传操纵系统 ; 实验平台 ; 模拟加载系统 ; 四余度EMA ; 半物理仿真
  • 英文关键词:airplane fly-by-wire system;;experimental platform;;simulation loading system;;four-redundancy EMA;;HIL simulation
  • 中文刊名:SYJL
  • 英文刊名:Experimental Technology and Management
  • 机构:中国民航大学航空自动化学院;
  • 出版日期:2015-10-14 09:25
  • 出版单位:实验技术与管理
  • 年:2015
  • 期:v.32;No.229
  • 基金:中国民航大学实验技术创新基金项目(17-13-01);; 中央高校基本科研业务费专项项目2013(3122013D022)
  • 语种:中文;
  • 页:SYJL201510029
  • 页数:6
  • CN:10
  • ISSN:11-2034/T
  • 分类号:113-118
摘要
为研究飞机电传操纵系统性能、给电传操纵系统设计提供实验依据,设计开发了飞机电传操纵及模拟加载系统实验台,实现全机飞控操纵系统半物理仿真。学生可以通过实验台操纵杆对飞机姿态进行调整,模拟飞机飞行过程中的姿态调整。并可完成永磁同步电机系统辨识、PID参数调试、电动加载模拟以及四余度方向舵故障模拟的实验,使学生更好熟悉四余度EMA机电作动器工作原理,为电传操纵系统的试验研究提供了平台。
        Experimental platform for airplane fly-by-wire and electric loading system is designed to study the performance of airplane fly-by-wire control system and provide the experimental basis for the system.Hardware-in-the-loop(HIL)simulation of airplane control system can be completed.Students can adjust the aircraft attitude by ajoystick of the experimental platform to simulate aircraft flight attitude adjustment.It can also do experiments such as permanent magnet synchronous motor system identification,parameter debugging in PID control,electric loading and the fault simulation of the four-redundancy aircraft rudder.It can make students better understand the four-redundancy EMA how to work.It also provide a platform for the research of fly-by-wire system.
引文
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