Multiple indicators optimization for stuffed Whipple shield ballistic limit equation
-
摘要: 为获得适用于国内填充式防护结构超高速撞击的弹道极限方程,采用多指标寻优的方法,对NASA填充式防护结构的弹道极限方程以国内实验数据为依据进行修正.结果发现:采用第1类指标(总体预测率和安全预测率)和第2类指标(预测误差平方和)联合对方程的系数进行修正,可获得预测效果更好的修正方程.通过对方程低速段和高速段的整体系数进行修正,最终获得单填充组、单一材料的双填充组以及两种材料的双填充组防护结构弹道极限方程的总体预测率分别为93.3%,90%和88.9%,而安全预测率全部高达100%,可很好满足工程的需求.可见,基于不同填充式防护结构的实验数据分别进行弹道极限方程的修正,可获得相应结构预测能力较优的方程.Abstract: In order to obtain the hypervelocity impact ballistic limit equation suiting for domestic stuffed Whipple shield, multiple indicators optimization method was studied. Based on domestic data, the NASA's ballistic limit equation of stuffed Whipple shield was revised. The results show that, joint the first kind of indicators(totality predicted rate and safety predicted rate) and the second kind of indicator (sum of squared prediction errors) together, better predicted equation can be obtained by correcting the coefficients of the stuffed Whipple shield ballistic limit equation. By correcting the coefficients of ballistic region and hypervelocity region, the corrected ballistic limit equations-totality predicted rate achieve 93.3%, 90% and 88.9% respectively for single-filled group, dual-filled group with single material and dual-filled group with two materials. And their safety predicted rate all reach up to 100%. So they can perfectly meet the engineering requirements. It is obvious that correcting the ballistic limit equations basing on experimental data for different kinds of stuffed Whipple shields, better predicted equations can be obtained for corresponding structures.
-
[1] 韩增尧,庞宝君.空间碎片防护研究最新进展[C]//第六届全国空间碎片学术交流会(上册).成都:国家国防科技工业局系统工程一司,2011:329-342 Han Zengyao,Pang Baojun.Latest progress of space debris protection[C]//The 6th National Academic Exchange on Space Debris(first volume).Chengdu:First Division of Systems Engineering,National Defense Science and Technology Industrial Development Bureau,2011:329-342(in Chinese) [2] Ryan S,Christiansen E L.Micrometeoroid and orbital debris (MMOD) shield ballistic limit analysis program[R].NASA/TM-2009-214789,2010 [3] Christiansen E L,Arnold J,Davis A,et al.Handbook for designing MMOD protection[R].NASA/TM-2009-214785,2009 [4] Christiansen E,Lambert M,Stokes H.IADC protection manual[M].Germany:Inter Agency Debris Committee,2002 [5] 张伟,庞宝君.航天器空间碎片防护方案的评价方法[J].中国空间科学技术,1998,18(006):30-36 Zhang Wei,Pang Baojun.Evaluation methods of space debris prevention scheme for spacecrafts[J].Chinese Space Science and Technology,1998,18(006):30-36(in Chinese) [6] 王应德,闫军,韩增尧,等.空间碎片防护用几种纤维材料的性能对比与SiC纤维的防护性能初步实验分析[C]//第六届全国空间碎片学术交流会(上册).成都:国家国防科技工业局系统工程一司,2011:357 Wang Yingde,Yan Jun,Han Zengyao,et al.Performance comparison of several fiber materials for space debris shields and preliminary experimental analysis of the protective properties about SiC fiber[C]//The 6th National Academic Exchange on Space Debris(first volume).Chengdu:First Division of Systems Engineering,National Defense Science and Technology Industrial Development Bureau,2011:357(in Chinese) [7] Christiansen E L,Crews J L,Williamsen J E,et al.Enhanced meteoroid and orbital debris shielding[J].International Journal of Impact Engineering,1995,17(1):217-228 [8] Christiansen E L,Kerr J H.Ballistic limit equations for spacecraft shielding[J].International Journal of Impact Engineering,2001,26(1):93-104 [9] 张宝玺.超高速撞击玄武岩及Kevlar纤维布填充防护结构优化设计[D].哈尔滨:哈尔滨工业大学航天学院,2011 Zhang Baoxi.The optimal structural design of stuffed shields with basalt and Kevlar fiber clothes on hypervelocity impacting[D].Harbin:School of Astronautics,Harbin Institute of Technology,2011(in Chinese) [10] 哈跃.玄武岩纤维材料及其填充防护结构超高速撞击特性研究[D].哈尔滨:哈尔滨工业大学航天学院,2009 Ha Yue.Research on hypervelocity impact properties of woven of basalt fibric and its stuffed shielding structure[D].Harbin:School of Astronautics,Harbin Institute of Technology,2009(in Chinese) [11] 徐小刚.航天器防护结构超高速撞击弹道极限方程综合建模方法研究[D].北京:北京航空航天大学宇航学院,2009 Xu Xiaogang.Ballistic limit equations integrated method of spacecraft shields under space debris hypervelocity impact[D].Beijing:School of Astronautics,Beijing University of Aeronautics and Astronautics,2009(in Chinese)
点击查看大图
计量
- 文章访问数: 1420
- HTML全文浏览量: 221
- PDF下载量: 561
- 被引次数: 0