Aircraft Longitudinal Auto-landing Guidance Law Using Time Delay Control Scheme

被引：9

作者：

Choi, Hyoung Sik ^{[1
]}

Lee, Sangjong ^{[1
]}

Lee, Jangho ^{[1
]}

Kim, Eung Tai ^{[1
]}

Shim, Hyunchul ^{[2
]}

机构：

[1] Korea Aerosp Res Inst, Taejon, South Korea

[2] Korea Adv Inst Sci & Technol, Dept Aerosp Engn, Taejon 305701, South Korea

来源：

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 2010年 / 53卷 / 181期

关键词：

Aircraft; Guidance and Control; Auto landing; Time Delay Control; Turbulence; ROBOT;

D O I：

10.2322/tjsass.53.207

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The objective of this paper is applying the Time Delay Control scheme for the aircraft auto-landing guidance problem A stability and control augmentation system and longitudinal auto landing guidance law using Time delay Control is proposed and evaluated through a simulation with model uncertainties and wind disturbances The proposed Time Delay Control guidance law shows good performance and is robust to model uncertainties and disturbances

引用

页码：207 / 214

页数：8

共 12 条

[1]

Blakelock J. H., 1991, AUTOMATIC CONTROL AI, P88

[2] A model reference observer for time-delay control and its application to robot trajectory control [J].