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考虑机构柔性的可重复使用运载器海上着陆动力学分析

杨少斐 张明 阮爽 雷波

南京航空航天大学学报(英文版)2026,Vol.43Issue(2):238-250,13.
南京航空航天大学学报(英文版)2026,Vol.43Issue(2):238-250,13.DOI:10.16356/j.1005-1120.2026.02.006

考虑机构柔性的可重复使用运载器海上着陆动力学分析

Analysis of Sea-Based Landing Dynamics of Reusable Landing Vehicle Considering Mechanism Flexibility

杨少斐 1张明 2阮爽 3雷波1

作者信息

  • 1. 南京航空航天大学航空航天结构力学及控制全国重点实验室,南京 210016,中国
  • 2. 南京航空航天大学航空航天结构力学及控制全国重点实验室,南京 210016,中国||南京航空航天大学飞行器先进设计技术国防重点学科实验室,南京 210016,中国
  • 3. 湖北航天技术研究院总体设计所,武汉 430040,中国
  • 折叠

摘要

Abstract

Vertical landing and recovery of a launch vehicle at sea can further reduce the launch cost of commercial space-flight,so this paper investigates the issue of reusable launch vehicle landing at sea.A vehicle landing dynamics model considering mechanism flexibility is established,and vehicle drop tests under various operating conditions are conducted.By comparing the vehicle drop test,the simulations of the dynamics model are consistent with test results,and the vehicle landing dynamics model considering the landing mechanism flexibility can simulate the vertical landing process of the vehicle more effectively than the rigid body dynamics model,which is more meaningful to guide the design of the reusable vehicle landing mechanism.Based on the vehicle landing dynamics model,a deck motion model and wind disturbance model are added to simulate the vehicle vertical landing dynamics at sea.The simulation results show that the sea landing causes the peak acceleration response of the vehicle,the main strut load and the buffer compression stroke to become larger,and there is a significant decrease in the landing stability of the vehicle.

关键词

可重复使用运载器/着陆动力学/落震试验/刚柔耦合模型/海上着陆

Key words

reusable landing vehicle/landing dynamics/drop test/rigid-flexible coupling model/sea-based landing

分类

航空航天

引用本文复制引用

杨少斐,张明,阮爽,雷波..考虑机构柔性的可重复使用运载器海上着陆动力学分析[J].南京航空航天大学学报(英文版),2026,43(2):238-250,13.

基金项目

This research was supported by the National Natural Science Foundation of China(No.12502042),the Postdoctoral Fellowship Program of China Postdoctoral Science Foundation(No.GZC20252752),and Jiangsu Funding Program for Excellent Postdoctoral Talent. (No.12502042)

南京航空航天大学学报(英文版)

1005-1120

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