APPLICATION OF MULTIOBJECTIVE OPTIMIZATION IN AIRCRAFT CONTROL-SYSTEMS DESIGN

被引：26

作者：

TABAK, D

SCHY, AA

GIESY, DP

JOHNSON, KG

机构：

[1] NASA,LANGLEY RES CTR,DIV FLIGHT DYNAM & CONTROL,STABIL & CONTROL BRANCH,HAMPTON,VA 23665

[2] VOUGHT CORP,HAMPTON TECH CTR,HAMPTON,VA

来源：

AUTOMATICA | 1979年 / 15卷 / 05期

关键词：

aircraft lateral control; Computer-aided design; multiobjective optimization; Pareto-optimality;

D O I：

10.1016/0005-1098(79)90007-4

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Multiobjective optimization techniques are applied in the design of an aircraft lateral control system. A large manned reentry vehicle and a fighter aircraft are considered. An algorithm suggested by Lin's Proper Inequality Constraints method, is implemented in the numerical computation of Pareto-optimal solutions. Subsequently, a trade-off analysis of several Pareto-optimal solutions is conducted. © 1979.

引用

页码：595 / 600

页数：6

共 15 条

[1]

Blakelock J., 1965, AUTOMATIC CONTROL AI

[2]

Etkin B., 1972, DYNAMICS ATMOSPHERIC, P134

[3] PROPER EFFICIENCY AND THEORY OF VECTOR MAXIMIZATION [J].