火箭技术

固冲发动机推力测量系统动态建模与分析

  • 谢海刚 ,
  • 李纲
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  • 中国空空导弹研究院, 河南洛阳 471009

谢海刚(1984-),男,河南洛阳人,工程师,硕士,研究方向:动态参数测量技术。

收稿日期: 2015-11-08

  网络出版日期: 2025-05-30

基金资助

空装预研课题

Dynamically Modeling and Analysis of Thrust Measurement System for Solid Ramjet

  • XIE Haigang ,
  • LI Gang
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2015-11-08

  Online published: 2025-05-30

摘要

针对固冲发动机地面试验中点火过程推力测量信号失真的问题,对推力测量系统进行了动态建模。采用ARMAX模型为基础的试验建模方法,设计实施了辨识试验,得到了不同激励下的响应信号。依据试验结果辨识出了模型的结构与阶次,建立了推力测量系统的动态模型。通过分析模型适配率和评估残差白色性,验证了模型准确有效。时域和频域分析结果表明,该动态模型可真实反映推力测量系统的动态特性,为改善动态特性、增加推力补偿和恢复真实信号奠定了基础。

本文引用格式

谢海刚 , 李纲 . 固冲发动机推力测量系统动态建模与分析[J]. 弹箭与制导学报, 2016 , 36(3) : 73 -77,81 . DOI: 10.15892/j.cnki.djzdxb.2016.03.020

Abstract

For ignition thrust measurement distortion of solid ramjet in ground test, a dynamic model for thrust measurement system was built.The responses at different excitation signals were obtained by designing and implementing identification test which based on ARMAX model.According to the test results, structure and order were identified and the dynamic model for thrust measurement system was built.Veracity and effectiveness of model were verified by fitting rate analysis and residual whiteness estimation.Time-frequency domain analysis results show that the dynamic model could be used to reflect actual dynamic characteristics of thrust measurement system, laying a foundation for improvement of dynamic characteristics, adding thrust compensation and real signals resume.

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