AIRCRAFT DESIGN FOR MISSION PERFORMANCE USING NONLINEAR MULTIOBJECTIVE OPTIMIZATION METHODS

被引：8

作者：

DOVI, AR

WRENN, GA

机构：

[1] Lockheed Engineering and Sciences Company, Hampton, VA

来源：

JOURNAL OF AIRCRAFT | 1990年 / 27卷 / 12期

基金：

美国国家航空航天局;

关键词：

D O I：

10.2514/3.45979

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A new technique that converts a constrained optimization problem to an unconstrained one where conflicting figures of merit may be simultaneously considered has been combined with a complex mission analysis system. The method is compared with existing single and multiobjective optimization methods. A primary benefit from this new method for multiobjective optimization is the elimination of separate optimizations for each objective, which is required by some optimization methods. A typical wide-body transport aircraft is used for the comparative studies.

引用

页码：1043 / 1049

页数：7

共 16 条

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