CAJ | 학술논문

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EM A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。
위연구비궤전전조종계통성능、급전전조종계통설계제공실험의거，설계개발료비궤전전조종급모의가재계통실험태，실현전궤비공조종계통반물리방진。학생가이통과실험태조종간대비궤자태진행조정，모의비궤비행과정중적자태조정。병가완성영자동보전궤계통변식、PID삼수조시、전동가재모의이급사여도방향타고장모의적실험，사학생경호숙실사여도EM A궤전작동기공작원리，위전전조종계통적시험연구제공료평태。
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 a joystick 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 .