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直升机扫雷系统跨介质刚柔耦合建模与配平分析

王洛烽 陈仁良 冯瑞

航空学报2025,Vol.46Issue(22):78-91,14.
航空学报2025,Vol.46Issue(22):78-91,14.DOI:10.7527/S1000-6893.2025.31900

直升机扫雷系统跨介质刚柔耦合建模与配平分析

Cross-medium rigid-flexible coupled modeling and trim analysis of helicopter mine-clearing system

王洛烽 1陈仁良 1冯瑞1

作者信息

  • 1. 南京航空航天大学 直升机动力学全国重点实验室,南京 210016||南京航空航天大学 直升机研究院,南京 210016
  • 折叠

摘要

Abstract

Naval mines present a severe threat to maritime safety.Helicopter-based mine clearing,compared to tradi-tional ship-based methods,offers faster deployment,higher efficiency,and lower risk.However,there is still a lack of publicly available modeling theories and analytical methods applicable to such systems.This paper establishes a cross-medium large-flexible towing cable model based on the absolute node coordinate formulation.Additionally,a rigid-body dynamics model for the helicopter and towing body,which facilitates easy coupling integration,is developed.The cross-medium rigid-flexible coupling model for the helicopter mine-clearing system is constructed and validated.A partitioned trim method for the coupled system is proposed,and the effects of key design and flight parameters on trim characteristics are analyzed.Results show that as flight speed increases,the helicopter nose-down attitude intensifies,while placing the towing point behind and above the center of gravity improves the attitude.During turns,the towing cable tension suppresses helicopter roll motion,requiring additional lateral control to provide centripetal force for turn-ing.Lower flight altitude and longer cables are ineffective at significantly increasing the depth of the towing body,ne-cessitating the installation of sinking components on the towing body.

关键词

飞行动力学/直升机扫雷/直升机拖曳/拖缆/拖体/耦合系统/配平方法

Key words

flight dynamics/helicopter mine-clearing/helicopter towing/towing cable/towing body/coupled sys-tem/trim method

分类

航空航天

引用本文复制引用

王洛烽,陈仁良,冯瑞..直升机扫雷系统跨介质刚柔耦合建模与配平分析[J].航空学报,2025,46(22):78-91,14.

基金项目

直升机动力学全国重点实验室基金(2023-HA-LB-067-01) (2023-HA-LB-067-01)

中国博士后科学基金(2023M741678) (2023M741678)

航空科学基金(ASFC-20240013052004) (ASFC-20240013052004)

江苏省卓越博士后计划资助 ()

江苏高校优势学科建设工程资助项目 National Key Laboratory Foundation of Helicopter Aeromechanics(2023-HA-LB-067-01) (2023-HA-LB-067-01)

China Postdoctoral Science Foundation(2023M741678) (2023M741678)

Aerospace Science Foundation of China(ASFC-20240013052004) (ASFC-20240013052004)

Jiangsu Funding Program for Excellent Postdoctoral Talent ()

A Project Funded by the Priority Academic Program Development of Jiangsu Higher Education Institutions ()

航空学报

OA北大核心

1000-6893

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