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References (37)
-
Shuai Yue, H. Nie, Ming Zhang, Mingyang Huang, Dafu Xu (2018)
Optimization and Performance Analysis of Oleo-Honeycomb Damper Used in Vertical Landing Reusable Launch VehicleJournal of Aerospace Engineering, 31
-
A. Pokaad, Md Said (2015)
The Effect of Mesh Size And Frictional Force on Simulation of Aluminium Honeycomb Under Quasi-Static LoadingApplied Mechanics and Materials, 786
-
Buffer characteristics of multistage honeycomb panels subjected to impact loads
Transactions of the Japan Society of Mechanical Engineers Series A, 61
-
M. Mahmoudabadi, M. Sadighi (2011)
A study on the static and dynamic loading of the foam filled metal hexagonal honeycomb – Theoretical and experimentalMaterials Science and Engineering A-structural Materials Properties Microstructure and Processing, 530
-
Xiao-Ming Fu, Lei Lei, Gang Yang, Baoren Li (2018)
Multi-objective shape optimization of autonomous underwater glider based on fast elitist non-dominated sorting genetic algorithmOcean Engineering
-
Guang Zheng, H. Nie, Jinbao Chen, Chuanzhi Chen, H. Lee (2018)
Dynamic analysis of lunar lander during soft landing using explicit finite element methodActa Astronautica
-
A. Ronch, M. Panzeri, M. Bari, R. D'Ippolito, M. Franciolini (2017)
Adaptive design of experiments for efficient and accurate estimation of aerodynamic loadsAircraft Engineering and Aerospace Technology, 89
-
Yuanyuan Liu, Shunguang Song, Ming Li, Chunjie Wang (2017)
Landing stability analysis for lunar landers using computer simulation experimentsInternational Journal of Advanced Robotic Systems, 14
-
I. Iváñez, L. Fernández-Cañadas, S. Sanchez-Saez (2017)
Compressive deformation and energy-absorption capability of aluminium honeycomb coreComposite Structures, 174
-
R. Oftadeh, B. Haghpanah, J. Papadopoulos, A. Hamouda, H. Nayeb-Hashemi, A. Vaziri (2014)
Mechanics of anisotropic hierarchical honeycombsInternational Journal of Mechanical Sciences, 81
-
G.A. Zupp, H.H. Doiron (1971)
A mathematical procedure for predicting the touchdown dynamics of a soft-landing vehicle -
Bo-Siou Wei (2008)
Research of the Factors of Buffering Performance in Lunar Lander -
S.-T. Hong, J. Pan, T. Tyan, P. Prasad (2006)
Quasi-static crush behavior of aluminum honeycomb specimens under compression dominant combined loadsInternational Journal of Plasticity, 22
-
M. Nohmi, A. Miyahara, Exploration Tsukuba (2005)
Modeling for Lunar Lander by Mechanical Dynamics Software -
Yuliang Lin, Zhifeng Zhang, Rong Chen, Yan Li, X. Wen, F. Lu (2015)
Cushioning and Energy Absorbing Property of Combined Aluminum HoneycombAdvanced Engineering Materials, 17
-
Ding Bei-chen (2013)
Numerical and experimental analyses on series aluminum honeycomb structures under quasi-static loadJournal of Vibration and Shock
-
Chen Wang, H. Nie, Jinbao Chen, H. Lee (2019)
The design and dynamic analysis of a lunar lander with semi-active controlActa Astronautica
-
M. Yamashita, M. Gotoh (2005)
Impact behavior of honeycomb structures with various cell specifications—numerical simulation and experimentInternational Journal of Impact Engineering, 32
-
运来 邓, 科达 姜, 郴祁 雷 (2014)
铝蜂窝材料动态压缩力学性能及吸能分析 A Study on Dynamic Compressive Mechanical Behaviors of Aluminum HoneycombsMaterial Sciences, 2014
-
(2017)
Energy-absorption and impact stability of series honeycombs -
Yangyang Dong, Tongxi Yu, Zijian Zhang (2020)
Mechanical design and energy absorption analysis of spherical honeycomb core for soft-landing device buffer shellActa Mechanica, 231
-
G. Aravind, S. Vishnu, K. Amarnath, U. Hithesh, P. Harikrishnan, Pramod Sreedharan, G. Udupa (2020)
Design, Analysis and Stability testing of Lunar Lander for Soft-LandingMaterials Today: Proceedings, 24
-
(2013)
Crashworthiness optimization of different topological structures of mental honeycomb used in a legged-typed lander -
Li Meng (2009)
Research on Cushion Properties and its Evaluation Methods of Legged-type Lander's Shock Absorber -
(2017)
The effect of pre-compression on the energy absorption of honeycomb cardboard -
Zhonggang Wang, Jie-fu Liu, Zhai-jun Lu, D. Hui (2017)
Mechanical behavior of composited structure filled with tandem honeycombsComposites Part B-engineering, 114
-
G. Liaghat, A. Alavinia (2003)
A comment on the axial crush of metallic honeycombs by Wu and JiangInternational Journal of Impact Engineering, 28
-
Xiong Zhang, Hui Zhang (2013)
Theoretical and numerical investigation on the crush resistance of rhombic and kagome honeycombsComposite Structures, 96
-
L. Dongping, Chai Hongyou, Zeng Fu-ming (2013)
Nonlinear finite element modeling and simulation for landing leg of lunar landerJournal of Beijing University of Aeronautics and Astronautics
-
Chen Yili (2011)
Mechanical properties of triangular honeycombs under in-plane impact loadingJournal of Vibration and Shock
-
Wang Hai-tao (2011)
Soft Landing Dynamics Simulation for Lunar Explorer -
Zhang Xin-chang (2012)
Effective Cushioning of Paper Honeycomb Material and Precompression TestPackaging Engineering
-
C. Tola, M. Nikbay (2018)
Solid rocket motor design using a surrogate modelAircraft Engineering and Aerospace Technology
-
(2017)
In-plane dynamic impact response characteristics of periodic 4-point star-shaped honeycomb structures -
H. Wu, W. Niu, Shuxin Wang, Shaoze Yan, Tao Liu (2020)
Sensitivity analysis of input errors to motion deviations of underwater glider based on optimized response surface methodologyOcean Engineering
-
(2012)
Energy absorption characteristics of a square hole honeycomb sandwich plate under blast loading -
M. Li, Z. Deng, Hongwei Guo, Rongqiang Liu, Bei-chen Ding (2014)
Optimizing crashworthiness design of square honeycomb structureJournal of Central South University, 21
- Publisher
- Emerald Publishing
- Copyright
- © Emerald Publishing Limited
- ISSN
- 1748-8842
- eISSN
- 1748-8842
- DOI
- 10.1108/aeat-02-2021-0043
- Publisher site
- See Article on Publisher Site
Abstract
In the field of planetary exploration, the legged-type lander is a common landing buffer device. There are two important performance metrics for legged-type landers: the energy absorption capacity and landing stability. In this paper, a novel method is proposed to optimize the honeycomb buffer of a legged-type lander. Optimization design variables are the dimension parameters of honeycomb and the objective functions are the evaluation parameters of the above two performance metrics.Design/methodology/approachA multi-body dynamic model of a lander and a finite-element model of the metal honeycomb are established. Based on the simulation results of the finite-element model and the quartic polynomial, the surrogate models are established to evaluate the energy absorption capacity of honeycomb. Considering both the multi-body dynamic model and the surrogate models, the study designed the optimization flow of dimension parameters of honeycomb. Besides, the non-dominated sorting genetic algorithm II is used for iterative calculation.FindingsImages of surrogate models show the monotonous functional relationship between the honeycomb’s energy absorption characteristics and its dimension parameters. Optimization results show an apparent contradiction among the objective functions. Besides, according to the simulation results, this method can significantly improve the comprehensive performance of the lander.Originality/valueThe novel method can effectively reduce the cost of honeycomb compression tests and improve the lander’s design. Therefore, it can be used for optimizing buffers of other types of legged-type landers.
Journal
Aircraft Engineering and Aerospace Technology: An International Journal – Emerald Publishing
Published: Aug 5, 2021
Keywords: Optimization design; Dynamics analysis; Surrogate model; Finite-element model; Honeycomb buffer; Legged-type lander