Approximations for quantitative feedback theory designs

被引：4

作者：

Henderson, DK ^{[1
]}

Hess, RA ^{[1
]}

机构：

[1] UNIV CALIF DAVIS,DEPT MECH & AERONAUT ENGN,DAVIS,CA 95616

来源：

JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 1997年 / 20卷 / 04期

关键词：

D O I：

10.2514/2.4122

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Quantitative feedback theory (QFT) is a powerful technique for the design of multi-input/multi-output (MIMO) flight control systems, which guarantees performance and stability robustness in the presence of significant parametric uncertainty in the vehicle model. The performance specifications can be stated in either time or frequency domain, with the latter being more common. The computational requirements for obtaining the results discussed are very modest and are easily accomplished using computer-aided control system design software.

引用

页码：828 / 831

页数：4