Hypervelocity impact damage prediction of stuffed Whipple shield based on Adaboost

被引:0
|
作者
Ding W. [1 ]
Li X. [2 ]
Yang H. [1 ]
机构
[1] Graduate School, Space Engineering University, Beijing
[2] Department of Aerospace Science and Technology, Space Engineering University, Beijing
关键词
Adaboost algorithm; Damage research; Safety prediction rate; Stuffed Whipple shield; Totality prediction rate;
D O I
10.13700/j.bh.1001-5965.2018.0216
中图分类号
学科分类号
摘要
The explicit ballistic limit equation of stuffed Whipple shield may cause some deviations between the prediction results and the measured data when the projectile is subjected to hypervelocity impact damage prediction because of different filling materials and filling methods. In this regard, the machine learning method is used to transform the problem into a binary problem. The projectile impact parameters and protective structure parameters in the collision process are used as the classification features to construct a hypervelocity impact damage prediction model of stuffed Whipple shield based on Adaboost. The model uses the classification and regression tree (CART) as a weak classifier to generate a strong classifier by weighted combination of a series of weak classifiers. Through the cyclic use of training samples, the impact damage prediction under a small sample set is achieved. The experimental results show that the established Adaboost prediction model has good prediction effect on the hypervelocity impact damage of stuffed Whipple shield. Both the totality prediction rate and the safety prediction rate of Adaboost prediction model increase by 14.3% compared with NASA's ballistic limit equation, and the established model has more versatility. Cross check under different training sample sizes proves that the model has good robustness and accuracy. © 2019, Editorial Board of JBUAA. All right reserved.
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页码:149 / 158
页数:9
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共 20 条
  • [1] Whipple F.L., Meteorites and space travel, The Astronomical Journal, 52, (1947)
  • [2] Cour-Palais B.G., Piekutowski A.J., The multi-shock hypervelocity impact shield, Shock Compression of Condensed Matter-1991, pp. 979-982, (1992)
  • [3] Robinson J.H., Hayashida K.B., Double-plate penetration equations: NASA TM-2000-209907, (2000)
  • [4] Christiansen E.L., Crews J.L., Williamsen J.E., Et al., Enhanced meteoroid and orbital debris shielding, International Journal of Impact Engineering, 17, 1, pp. 217-228, (1995)
  • [5] Ryan S., Thaler S., Artificial neural networks for characterizing Whipple shield performance, Procedia Engineering, 58, 56, pp. 31-38, (2013)
  • [6] Liu S., Li Y., Huang J., Et al., Hypervelocity impact test results of Whipple shield for the validation of numerical simulation, Journal of Astronautics, 26, 4, pp. 505-508, (2005)
  • [7] Guan G.S., Hypervelocity impact characteristics investigation on the spacecraft space debris shield configuration, (2006)
  • [8] Zhang X.T., Shen Y., Jia G.H., Support vector machine model for spacecraft single wall ballistic limit prediction, Journal of Astronautics, 35, 3, pp. 298-305, (2014)
  • [9] Jia G.H., Ouyang Z.J., Jiang H., Et al., Multiple indicators optimization for stuffed Whipple shield ballistic limit equation, Journal of Beijing University of Aeronautics and Astronautics, 39, 12, pp. 1573-1583, (2013)
  • [10] Jia G.H., Ouyang Z.J., Jiang H., Analysis and instances of ballistic limit equations'predictive indicators, Acta Aeronautica et Astronautica Sinica, 34, 10, pp. 2364-2371, (2013)