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基于遥测力学环境参数的飞行器横向响应载荷辨识方法

刘学 李冬 徐洪洲 胡健

机械制造与自动化2026,Vol.55Issue(3):95-99,5.
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机械制造与自动化2026,Vol.55Issue(3):95-99,5.DOI:10.19344/j.cnki.issn1671-5276.2026.03.019

基于遥测力学环境参数的飞行器横向响应载荷辨识方法

Identification Method for Aircraft Lateral Response Loads Based on Telemetry Mechanical Environmental Parameters

刘学 1李冬 1徐洪洲 1胡健1

作者信息

  • 1. 中国人民解放军91550部队,辽宁大连 116023
  • 折叠

摘要

Abstract

Given the big error between the theoretical dynamic model and the actual situation caused by the complexity of the underwater mechanical environment of the submarine-launched aircraft,this paper proposes an identification method for lateral response loads of aircraft during water egress based on telemetry mechanical environment parameters.Based on the theory of structural mechanics,this method,first,identified the modal parameters of the telemetered mechanical environment parameters of the water-egress phase of the aircraft by combining the natural environment excitation technique with the eigensystem realization algorithm.Then,the vibration response of the key section was decomposed adaptively by the variational mode decomposition method to obtain the low-order modal response components,Finally,according to the principle of modal superposition and modal orthogonality theory,the modal coordinates were obtained by using the identified modal parameters and the low-order modal components.Also,the lateral response load was identified through the combination of the modal shear force and the modal bending moment.The actual measurement example verified the validity of the method.

关键词

力学环境参数/自然环境激励技术/特征系统实现算法/变分模态分解/载荷辨识

Key words

mechanical environment parameters/natural excitation technique/eigensystem realization algorithm/variational mode decomposition/load identification

分类

航空航天

引用本文复制引用

刘学,李冬,徐洪洲,胡健..基于遥测力学环境参数的飞行器横向响应载荷辨识方法[J].机械制造与自动化,2026,55(3):95-99,5.

基金项目

国家自然科学基金项目(61801482) (61801482)

中国博士后科研基金特别资助项目(2020T130772) (2020T130772)

机械制造与自动化

1671-5276

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