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2018, 02, No.188 56-59+101
An Optimum Method for Internal and External Ballistic Design Based on Uncertainty
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DOI: 10.16358/j.issn.1009-1300.2018.02.09
Abstract:

It is difficult to obtain the optimal solution because of the separation of internal and external ballistic design and conservative margin.An optimum method based uncertainty for internal and external ballistic design is present.Firstly,the uncertainty model of the solid engine is established,then uncertainty-based optimum methodology based "deviation allowance,margin free"is used to design ballistic.Three elements of optimization are given.A sort of software based on iSIGHT is developed.At last,an example is given to illustrate the application.With the constant of weight,range,the effectiveness of the method is effective.

References

[1]龙乐豪.导弹与航天丛书《总体设计》(上册)[M].北京:宇航出版社,1989:101-104.

[2]Zang T A,Michael J.Needs and opportunities for uncertainty-based multidisciplinary design methods for aerospace vehicles[R].NASA/TM-2002-211462,2002.

[3]Max Calabro,Alian Dufour.Optimization of the propulsion for multi-stage solid rocket motors launchers.IFA.97S.07.

[4]刘百奇.基于不确定性的固体运载器多学科优化方法[J].导弹与航天运载技术,2016,(1):1-4.

[5]蓝文博.基于i SIGHT的战术导弹多学科优化设计[J].战术导弹技术,2010,(4):80-84.

Basic Information:

DOI:10.16358/j.issn.1009-1300.2018.02.09

China Classification Code:TJ013;V412

Citation Information:

[1]Lv Yan,Liu Baiqi,Yin Shiming.An Optimum Method for Internal and External Ballistic Design Based on Uncertainty[J].Tactical Missile Technology,2018,No.188(02):56-59+101.DOI:10.16358/j.issn.1009-1300.2018.02.09.

Published:  

2018-03-15

Publication Date:  

2018-03-15

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