In-situ calibration data processing for gas controllable engine

Yi Guo*, Xiang Yang Liu, Guang Ke Zhang, Zhi Jun Wei, Ning Fei Wang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

The structure of the test system for gas controllable engine was introduced and the thrust test model was analyzed and established. The calibration data processing algorithms based on the simplified model and the precise model were proposed and the uncertainty was evaluated for both means. The results of the in-situ calibration data processing show that the simplified model algorithm can be used as a rough calibration data processing method as it's relative uncertainty is 2.06%. The precise model algorithm can get more precise calibration coefficients as the relative uncertainty is improved from 2.06% to 0.31%. In addition, the precise model algorithm can reflect some in-situ factors such as difference of channel sensitivity, coupled extent of moveable frame and position error, requiring less test-bed debugging work.

Original languageEnglish
Pages (from-to)659-662
Number of pages4
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume34
Issue number5
Publication statusPublished - Oct 2011

Keywords

  • Data processing
  • Gas controllable engine
  • In-situ calibration
  • Thrust test model

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