Performance investigation of high-altitude simulation cabin based on Labview

Jinfang Nie, Quan Pan, Dalin Zhang

科研成果: 期刊稿件文章同行评审

2 引用 (Scopus)

摘要

For the performance testing of cabin pressure control system (CPCS), a high-altitude simulation cabin (HASC) system based on the virtual instrument is established to simulate the atmospheric pressure which varies with aircraft flight states. On the basis of SCXI virtual instrument platform, a digital proportion-integration-differentation (PID) controller is developed in Labview to accomplish the HASC pressure control. The performance test of digital-pneumatic cabin pressure controlling system is carried out with the HASC system. The results show that the HASC system can accurately simulate the atmospheric pressure of flight states which is very important in CPCS performance tesing.

源语言英语
页(从-至)597-598
页数2
期刊Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics
46
4
出版状态已出版 - 1 8月 2014

指纹

探究 'Performance investigation of high-altitude simulation cabin based on Labview' 的科研主题。它们共同构成独一无二的指纹。

引用此