东北大学学报:自然科学版 ›› 2015, Vol. 36 ›› Issue (5): 626-630.DOI: 10.12068/j.issn.1005-3026.2015.05.005

• 信息与控制 • 上一篇    下一篇

基于综合赋权C-TOPSIS法的航天器研制风险控制

张志峰1, 白焱2   

  1. (1.西北工业大学 航天学院, 陕西 西安710072; 2.空军工程大学 防空反导学院, 陕西 西安710051)
  • 收稿日期:2014-04-09 修回日期:2014-04-09 出版日期:2015-05-15 发布日期:2014-11-07
  • 通讯作者: 张志峰
  • 作者简介:张志峰(1962-),男,陕西咸阳人,西北工业大学博士研究生,空军工程大学教授,博士生导师.
  • 基金资助:
    航空科学基金重点资助项目(20120469801).

Risk Control of the Spacecraft Development Based on Comprehensive Weight C-TOPSIS

ZHANG Zhi-feng1, BAI Yan2   

  1. 1. School of Astronautics,Northwestern Polytechnical University, Xi’an 710072,China; 2. Missile Institute, Air Force Engineering University, Xi’an 710051,China.
  • Received:2014-04-09 Revised:2014-04-09 Online:2015-05-15 Published:2014-11-07
  • Contact: BAI Yan
  • About author:-
  • Supported by:
    -

摘要: 通过对航天器研制风险评估指标的分析,建立基于综合赋权的逼近理想点法(TOPSIS)的风险控制模型.运用层次分析法(AHP)求得主观权重,熵值赋权法获得客观权重,再通过线性规划的方法求出综合权重;用“垂面射影法”替代现有相对欧式距离对TOPSIS法进行优化,提高了评估精度;对风险评价指标进行分类处理,建立分层评价指标体系,简化了运算过程.最后结合航天器研制风险控制实例,选出了较为优化的技术方案,证明了该方法的可行性.

关键词: 航天器研制, C-TOPSIS, 分类, 熵权法, 风险控制

Abstract: By analyzing the risk of the spacecraft developing evaluation index, a risk control model was built based on comprehensive weight TOPSIS. In this model, the subject and the object weight were calculated by AHP and entropy-weight method. The linear programming was used to count the comprehensive weight. And TOPSIS method was optimized by using “vertical plane projection method” to substitute existing opposite continental distance, resulting in improving the precision of evaluate. The risk evaluated target was clustered, and the different sort target system was set up, resulting in predigesting the process of the operation. In the end, the best scheme was selected by combining the example of spacecraft development control. The result showed the feasibility of the developed method.

Key words: spacecraft development, C-TOPSIS, clustering, entropy power process, risk control

中图分类号: