航空学报 > 1985, Vol. 6 Issue (6): 597-601

飞行模拟转台伺服系统的改进

孙德志   

  1. 航空精密机械工程研究所
  • 收稿日期:1984-05-01 修回日期:1900-01-01 出版日期:1985-12-25 发布日期:1985-12-25

IMPROVEMENT OF SERVO SYSTEMS FOR FLIGHT SIMULATOR

Sun Dezhi   

  1. China precision Engineering Institute for Aircraft Industry
  • Received:1984-05-01 Revised:1900-01-01 Online:1985-12-25 Published:1985-12-25

摘要: 在研制YMT-S1型飞行模拟转台(以下简称转台)的过程中,作者对转台的伺服系统作了大量的实验研究,在原有伺服系统的基础上进行了改进设计,构成了“双速”伺服系统、包含速度微分反馈的速度系统及位置系统、“综合”控制伺服系统。 实验证明:三种伺服系统对提高转台的技术性能有明显效果。 本文介绍了这三种伺服系统的构成、工作原理及效果。

Abstract: A great deal of experimental research on servo systems of simulator in developing YMT-S1 type flight simulator was carried out. A modification of its design was accomplished by improving "double velocity" servo system, velocity or position servo system with velocity differential feedback, and "integral control" servo system.The experiments have proved that these three types of servo system have tangible results in improving performances of the simulator.Their formation, working principles and results are presented.