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

作　　者：潘科[1,2] 潘宣宏 郭新奇[2] 何杨[1] 章志斌 

机构地区：[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

出　　处：《舰船电子工程》2017年第4期21-24,共4页Ship Electronic Engineering

基　　金：部委基础研究基金项目资助

摘　　要：针对空中加油机的设计参数对其作战效能的影响,基于空中加油机的自身性能和任务能力选取了影响其作战效能的设计参数,以世界现役几种典型空中加油机为评估样本的数据矩阵,用多元数据回归中的主成分分析方法对样本矩阵进行了统计分析,得出了一些有益的结论,为空中加油机的设计提供了依据,结果分析表明文中方法的可行性。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 

分 类 号：V271.4[航空宇航科学与技术—飞行器设计]