大载重气囊缓冲性能分析及多目标优化

Abstract
Figure/Table
References (17)
Related Citation (15)

Download: PDF (2265 KB) HTML (1 KB)
Export: BibTeX | EndNote (RIS)

Abstract

Buffering technology is one of the key technologies for spacecraft landing and recovery.It is of great significance to study reasonable reduction of spacecraft overload to the safety of human body and its internal equipment.Firstly, the validity of numerical simulation method was verified by comparing the results from the control volume with the testing of literature.Then, the buffering process of six combined airbags landing system was simulated for a heavy load module.The effects of the initial internal pressure, the open timing, and the area of the venting holes of external airbags on the buffering characteristics were further studied by single parameter variation.The criteria for evaluating the collision or rebound of the module were proposed.The sample points for simulation were selected by the optimal Latin hypercube design method in order to optimize the maximum overload and the specific absorption energy of the airbag landing system.The agent model of neural network was constructed according to the buffering characteristics.Finally, the initial parameters of the airbags were optimized by the multi-objective genetic algorithm.The results show that the maximum overload optimized reduces by 17.717%, and the module with the heavy load does not rebound.

Key words： heavy landing airbags specific absorption energy collision overload buffering multi-objective optimization

Received: 11 July 2019 Published: 15 December 2020

	Service

	E-mail this article
	Add to my bookshelf
	Add to citation manager
	E-mail Alert
	RSS
	Articles by authors
	ZHANG Pengfei1
	2
	WEI Jianzheng1
	CHEN Xueyan1
	TAN Huifeng1
	ZHU Meifang3

Cite this article:

ZHANG Pengfei1,2,WEI Jianzheng1, et al. Analysis and multi-objective optimization for buffer performance of heavy landing airbags[J]. JOURNAL OF VIBRATION AND SHOCK, 2020, 39(24): 91-98.

URL:

http://jvs.sjtu.edu.cn/EN/ OR http://jvs.sjtu.edu.cn/EN/Y2020/V39/I24/91

[1] 温金鹏,薛江,张思才,等. 固定排气口型气囊冲击减缓特性研究[J]. 振动、测试与诊断, 2018, 38(02): 387-393+425.
WENG Jinpeng, XUE Jiang, ZHANG Sicai, et al. Study on shock mitigation characteristics of fixed exhaust air bag[J]. Journal of Vibration, Measurement& Diagnosis, 2018, 38(02): 387-393+425.
[2] Cadogan D,Sandy C, Grahne M. Development and evaluation of the mars pathfinder inflatable airbag landing system[J]. Acta Astronautica, 2002, 50(10): 633-640.
[3] Turner C T, Girard L A. Air bag impact attenuation system for the AQM-34V remote piloted vehicle[J]. Journal of Aircraft, 1982, 19(11): 984-989. [4] Bown N W, Darley M G. Advanced Airbag Landing Systems for Planetary Landers[C]// 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. 2005: 1-16.
[4] Bown N W, Darley M G. Advanced Airbag Landing Systems for Planetary Landers[C]// 18th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. 2005: 1-16.
[5] Tutt B,Sandy C, Corliss J. Status of the Development of an Airbag Landing System for the Orion Crew Module[C]// 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. 2009: 1-13.
[6] Shook L S,Timmers R B, Hinkle J. Second Generation Airbag Landing System for the Orion Crew Module[C]// 20th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar. 2009: 1-8.
[7] 张华, 孟光, 刘汉武, 等. 行星软着陆气囊缓冲系统动力学仿真研究[J]. 振动与冲击, 2016, 35(20): 125-129+208.
ZHANG Hua, MENG Guang, LIU Hanwu, et al. Dynamics simulation on a planetary airbag buffering and landing system[J]. Journal of vibration and shock, 2016, 35(20): 125-129+208.
[8] 文桂林,肖久如,尹汉锋,等. 全向式多室连通火星着陆缓冲气囊的多目标优化设计[J]. 机械工程学报, 2015, 51(15): 135-141.
WEN Guilin, XIAO Jiuru, YIN Hanfeng, et al. Multi-objective Optimization Design of Omni-directional Multi-chamber Airbag for Land-ing on Mars[J]. Journal of mechanical engineering, 2015, 51(15): 135-141
[9] 洪煌杰,王红岩,李建阳, 等. 基于代理模型的空投装备气囊缓冲系统多目标优化[J]. 振动与冲击, 2015, 34(03): 215-220.
HONG Huangjie,WANG Hongyan,LI Jianyang, et al. Multi-objective optimization of an airbag cushion system for airdropping equipment based on surrogate model[J]. Journal of vibration and shock, 2015, 34(03): 215-220.
[10] 温金鹏, 李斌, 谭德伟, 等. 考虑织布弹性的软着陆气囊缓冲特性研究[J]. 振动与冲击,2010, 29(02): 79-83+110+222.
WEN Jin-peng，LI Bin，TAN De-wei，et al．Cushioning characteristics of a soft landing airbag with elastic fabric[J]. Journal of vibration and shock, 2010, 29(02): 79-83+110+222.
[11] 牛四波, 王红岩, 迟宝山, 等. 重装回收系统双气室气囊缓冲特性分析[J]. 振动与冲击, 2012, 31(10): 74-8+170.
NIU Si-bo, WANG Hong-yan, CHI Bao-shan, et al. Cushioning characteristics of double-chamber airbag for heavy equipment recovery system[J]. Journal of vibration and shock, 2012, 31(10): 74-8+170.
[12] 雷江利,荣伟,贾贺,等. 国外新一代载人飞船减速着陆技术研究[J]. 航天器工程, 2017, 26(1): 100-109.
LEI Jiangli, RONG Wei, JIA He, et al.Research on Descent and Landing Technology for New Generation Manned Spacecraft[J]. SPacecraft engineering, 2017, 26(1): 100-109.
[13] 李建阳, 周宇, 王红岩, 等. 组合型气囊参数对缓冲特性的影响分析[J]. 载人航天, 2018, 24(05): 568-573.
LI Jianyang, ZHOU Yu, WANG Hongyan, et al. Effects of Combined Airbag Parameters on Cushioning Characteristics[J]. Manned Spaceflight, 2018, 24(05): 568-573.
[14] 卫剑征, 王滢, 甄铎, 等. 气囊着陆缓冲过程仿真分析[J]. 载人航天, 2018, 24(04): 529-535.
WEI Jianzheng, WANG Ying, ZHEN Duo， et al. Simulation Analysis of Airbag Cushioning Process during Landing[J]. Manned Spaceflight, 2018, 24(04): 529-535.
[15] KIM H-S. New extruded multi-cell aluminum profile for maximum crash energy absorption and weight efficiency [J]. Thin-Walled Structures, 2002, 40(4): 311-27.
[16] 李彬, 庞永杰, 程妍雪, 等. 基于EBF 神经网络的复合材料耐压壳性能研究[J]. 哈尔滨工程大学学报, 2016, 37(10): 1323-1329.
LI Bin, PANG Yongjie, Cheng Yanxue， et al. Ｒesearch on a composite pressure hull based on an EBF neural network [J]. Journal of Harbin Engineering University, 2016, 37(10): 1323-1329.
[17] Yuanming Xu,Shuo Li, Xiaomin Rong. Composite Structural Optimization by Genetic Algorithm and Neural Network Response Surface Modeling[J]. Chinese Journal of Aeronautics, 2005, 18(4): 310-316.