首页|期刊导航|南京航空航天大学学报(英文版)|考虑机构柔性的可重复使用运载器海上着陆动力学分析

考虑机构柔性的可重复使用运载器海上着陆动力学分析OA

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

中文摘要英文摘要

运载器海上垂直着陆回收可以进一步减少商业航天的发射成本,因此对可重复使用运载器海上着陆问题进行了研究.首先建立了考虑着陆机构柔性化的运载器着陆动力学模型,并进行了多种工况下的运载器落震试验.通过对比运载器落震试验,动力学模型仿真与试验结果具有一致性,且考虑着陆机构柔性化的运载器着陆动力学模型相比刚体动力学模型可以更有效地模拟运载器垂直着陆过程,对可重复使用运载器着陆机构的设计更具有指导意义.在运载器着陆动力学模型基础上,添加了基于功率谱的甲板运动模型和运载器风扰模型,进行了运载器海上垂直着陆动力学仿真.仿真结果表明,海上着陆会使运载器加速度响应峰值、主支柱载荷与缓冲器压缩行程变大,且运载器的着陆稳定性有明显下降.

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.

杨少斐;张明;阮爽;雷波

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,中国湖北航天技术研究院总体设计所,武汉 430040,中国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

航空航天

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

reusable landing vehiclelanding dynamicsdrop testrigid-flexible coupling modelsea-based landing

《南京航空航天大学学报(英文版)》 2026 (2)

238-250,13

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.

10.16356/j.1005-1120.2026.02.006

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