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空中加油机作战效能设计参数的主成分分析

潘科 潘宣宏 郭新奇 何杨 章志斌

舰船电子工程2017,Vol.37Issue(4):21-24,4.
舰船电子工程2017,Vol.37Issue(4):21-24,4.DOI:10.3969/j.issn.1672-9730.2017.04.006

空中加油机作战效能设计参数的主成分分析

Principal Component Analysis on Design parameters of Aerial Refueling Aircraft Operational Effectiveness

潘科 1潘宣宏 2郭新奇 3何杨 2章志斌1

作者信息

  • 1. 海军指挥学院研究生队 南京 210016
  • 2. 海军航空工程学院指挥系 烟台 264001
  • 3. 海军指挥学院合同战术系 南京 210016
  • 折叠

摘要

Abstract

Since parameters analysis can analyze the effects of design parameters on Aerial refueling aircraft operational effectiveness,based of the performance and mission capability,this paper establishes the evaluation indexes collection of the aerial refueling aircraft and the index matrix of samples to be sorted,and uses the principal components analysis for construction an evaluation index of multi-index system and sorts the samples with this method, which provided the basis for the selection of parameters in the program design.Finally, some significant conclusion were educed, and the results show that the method is effective and feasible.

关键词

空中加油机/作战效能/主成分分析

Key words

carrier-based aircraft/operational effectiveness/principal component analysis

分类

航空航天

引用本文复制引用

潘科,潘宣宏,郭新奇,何杨,章志斌..空中加油机作战效能设计参数的主成分分析[J].舰船电子工程,2017,37(4):21-24,4.

基金项目

部委基础研究基金项目资助 ()

舰船电子工程

OACSTPCD

1672-9730

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