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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1990, Vol. 11 ›› Issue (2): 101-106.

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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

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