航空学报 > 1990, Vol. 11 Issue (2): 101-106

舱温系统的分析及控制方案的改进

赵民生   

  1. 中国民航学院
  • 收稿日期:1988-04-20 修回日期:1900-01-01 出版日期:1990-02-25 发布日期:1990-02-25

ANALYSIS AND IMPROVEMENT OF CABIN TEMPERATURE CONTROL SYSTEM

China Zhao Minsheng   

  1. Civil Aeronautics Institute of China
  • Received:1988-04-20 Revised:1900-01-01 Online:1990-02-25 Published:1990-02-25

摘要: <正> 1.前言 舱温系统是一个恒值系统,为了保证恒值系统的稳态精度是容易的,因为系统中的执行电机已经包含了一个积分环节。但系统中座舱时间常数很大,使得系统的动态过程波动性很大。回顾舱温系统的发展过程,可以看出系统每一次重大改进都是围绕改善系统的动特性进行的。例如早期双金属继电式舱温系统发展为延迟负反馈继电式舱温系统,就是利用振荡线性化的方法使继电器成为线性特性,因而减少了系统的振荡。以后系统中采用了预感电桥,增加了系统的稳定性。但由于超前的时间常数无法作的很大,不能有效地补偿座舱惯性造成的时间延迟。所以动态特性仍然不能令人满意,再加上飞行过程中不断受到干扰以至舱温总是处于波动状态。

关键词: 振荡线性化, 预感电桥, 顺馈

Abstract: In this paper, a linearized mathematical model of the delayed negative feedback oscillation is derived. In order to improve the sta-bility and disturbance rejection o.f the cabin temperature control system,a new approach to the design of pre-sensing bridge circuit is presented. The pro-sensing brige so designed can realise a lead-correction with time-constant as high as a few thousand seconds. Besides,by employing the existing engine control system installations, without any additional parts a feedforward control method for rejecting disturbance can be achieved.

Key words: oscillation linearization, pre-sensing bridge, feed-forward control