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某靶标助推段横侧向大过载振荡分析

王磊 高浩 柳长安 李家乐

火箭推进2025,Vol.51Issue(5):56-62,7.
火箭推进2025,Vol.51Issue(5):56-62,7.DOI:10.3969/j.issn.1672-9374.2025.05.006

某靶标助推段横侧向大过载振荡分析

Analysis of the large amplitude lateral vibration in a certain target's booster phase

王磊 1高浩 1柳长安 1李家乐1

作者信息

  • 1. 西安航天动力研究所,陕西 西安 710100||西安市高速飞行器攻防对抗技术及应用重点实验室,陕西 西安 710072
  • 折叠

摘要

Abstract

There is a kind of large amplitude lateral vibration in a certain target's booster phase,which may cause some faults to missions.In order to analyse how the lateral vibration comes into being,some telemeter data signal processing and analysis are made to recognise the vibration characters and the relationships between the telemeter data.Then,by comparing the vibration characters with the structure vibration modes,the lateral vibration can be confined to some lateral band vibration mode patterns.At last,with the help of the flight simulation analyses,it is shown that the lateral vibration is affected by the yaw channel,which is excited by the rolling control as the target's coupled aerodynamic characteristics,and as a result,the additional accelerations are detected by the inertial components.

关键词

靶标/短时傅里叶变换/振动模态/阶跃激励/周期性激励

Key words

target/short-time Fourier transform/vibration mode/step excitation/periodic excitation

引用本文复制引用

王磊,高浩,柳长安,李家乐..某靶标助推段横侧向大过载振荡分析[J].火箭推进,2025,51(5):56-62,7.

基金项目

中国航天科技集团科技创新项目(2014qj.htyq-1tm) (2014qj.htyq-1tm)

火箭推进

OA北大核心

1672-9374

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