Integrated aircraft-controller design using linear matrix inequalities

被引：27

作者：

Niewoehner, RJ

Kaminer, II

机构：

[1] U.S. Naval Postgraduate School, Monterey

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1996年 / 19卷 / 02期

关键词：

D O I：

10.2514/3.21638

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A new methodology is presented for solving the problem of optimizing the aircraft parameters, such as the size of its control surfaces, while meeting open- and closed-loop static and dynamic performance requirements. The approach proposed involves rewriting these requirements as linear matrix inequalities and solving a related constrained optimization problem for which efficient numerical solutions are available.

引用

页码：445 / 452

页数：8

共 19 条

[1]

BOYD S, 1994, STUDIES APPLIED MATH, V15

[2]

DOYLE J, 1991, FEEDBACK CONTROL THE

[3]

GAHINET P, 1993, PROCEEDINGS OF THE 32ND IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4, P656, DOI 10.1109/CDC.1993.325066

[4]

GAHINET P, 1993, PROCEEDINGS OF THE 32ND IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4, P3162, DOI 10.1109/CDC.1993.325785

[5]

GOH KC, 1994, PROCEEDINGS OF THE 1994 AMERICAN CONTROL CONFERENCE, VOLS 1-3, P850

[6]

HOAK DE, 1960, USAF STABILITY CONTR

[7] ACTIVE CONTROL TECHNOLOGY FOR LARGE SPACE STRUCTURES [J].

HYLAND, DC ;

JUNKINS, JL ;

LONGMAN, RW .

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1993, 16 (05) :801-821

[8]

Jameson A., 1988, Journal of Scientific Computing, V3, P233, DOI 10.1007/BF01061285

[9]

JUNKINS JL, 1990, MECHANICS CONTROL LA, V129, pCH3

[10] MIXED H-2/H-INFINITY CONTROL - A CONVEX-OPTIMIZATION APPROACH [J].

KHARGONEKAR, PP ;

ROTEA, MA .

IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1991, 36 (07) :824-837

← 1 2 →