PRACTICAL CONTROL LAW DESIGN FOR AIRCRAFT USING MULTIVARIABLE TECHNIQUES

被引：66

作者：

BLIGHT, JD

DAILEY, RL

GANGSAAS, D

机构：

[1] Boeing Defense and Space Group, Seattle, WA, 98124

来源：

INTERNATIONAL JOURNAL OF CONTROL | 1994年 / 59卷 / 01期

关键词：

D O I：

10.1080/00207179408923071

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Several applications and adaptations of multivariable control theory for aircraft control law developments are described. Applications include solution of a lateral oscillation problem in the Boeing 767 autopilot, a longitudinal control law giving excellent handling qualities for stable or unstable airframes, and a high-agility fighter giving superior flying qualities up to 90 degrees angle of attack. Adaptations of control theory include meeting the Gibson longitudinal flying qualities criterion, a unified application of linear quadratic design theory, and application of the structured singular value. The paper also includes a discussion of the Boeing software tools used for model building, control analysis and design.

引用

页码：93 / 137

页数：45

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