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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OA

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

中文摘要英文摘要

针对潜射飞行器水下力学环境的复杂性导致理论动力学模型与实际情况误差较大的问题,提出一种基于遥测力学环境参数的飞行器出水横向响应载荷辨识方法.以结构动力学理论为基础,采用自然环境激励技术法联合特征系统实现算法对飞行器出水段的遥测力学环境参数进行模态参数辨识;利用变分模态分解方法对关键截面的振动响应进行自适应分解获取其低阶模态响应分量;根据模态叠加原理和模态正交理论,利用辨识的模态参数和低阶模态分量求取其模态坐标,结合模态剪力和模态弯矩进行横向响应载荷识别.实测算例验证了该方法的有效性.

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.

刘学;李冬;徐洪洲;胡健

中国人民解放军91550部队,辽宁大连 116023中国人民解放军91550部队,辽宁大连 116023中国人民解放军91550部队,辽宁大连 116023中国人民解放军91550部队,辽宁大连 116023

航空航天

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

mechanical environment parametersnatural excitation techniqueeigensystem realization algorithmvariational mode decompositionload identification

《机械制造与自动化》 2026 (3)

95-99,5

国家自然科学基金项目(61801482)中国博士后科研基金特别资助项目(2020T130772)

10.19344/j.cnki.issn1671-5276.2026.03.019

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