Glideslope capture in wind gust via fuzzy logic controller

Kyungmoon Nho; Ramesh K. Agarwal

Glideslope capture in wind gust via fuzzy logic controller

Research output: Contribution to conference › Paper › peer-review

Abstract

Fuzzy logic based control system is developed for glideslope capture of an aircraft under gust. First, the design of a longitudinal control system for automatic landing is presented for a linear aircraft model. Then, the fuzzy controller parameters derived for the linear model are modified to obtain a robust control system for a six degree of freedom nonlinear aircraft model. It is shown that the simple tuning fuzzy controller, by altering scaling factors, is well suited for control of difficult aircraft maneuvers like landing in severe weather conditions which require continuous change in engine thrust and control surfaces.

Original language	English
State	Published - 1999
Event	37th Aerospace Sciences Meeting and Exhibit, 1999 - Reno, United States Duration: Jan 11 1999 → Jan 14 1999

Conference

Conference	37th Aerospace Sciences Meeting and Exhibit, 1999
Country/Territory	United States
City	Reno
Period	01/11/99 → 01/14/99

Cite this

@conference{44596a59fadf47c69b7eef8c00edc3da,

title = "Glideslope capture in wind gust via fuzzy logic controller",

abstract = "Fuzzy logic based control system is developed for glideslope capture of an aircraft under gust. First, the design of a longitudinal control system for automatic landing is presented for a linear aircraft model. Then, the fuzzy controller parameters derived for the linear model are modified to obtain a robust control system for a six degree of freedom nonlinear aircraft model. It is shown that the simple tuning fuzzy controller, by altering scaling factors, is well suited for control of difficult aircraft maneuvers like landing in severe weather conditions which require continuous change in engine thrust and control surfaces.",

author = "Kyungmoon Nho and Agarwal, {Ramesh K.}",

note = "Publisher Copyright: {\textcopyright} 1998 by Kyungmoon Nho and Ramesh K. Agarwal.; 37th Aerospace Sciences Meeting and Exhibit, 1999 ; Conference date: 11-01-1999 Through 14-01-1999",

year = "1999",

language = "English",

}

TY - CONF

T1 - Glideslope capture in wind gust via fuzzy logic controller

AU - Nho, Kyungmoon

AU - Agarwal, Ramesh K.

PY - 1999

Y1 - 1999

N2 - Fuzzy logic based control system is developed for glideslope capture of an aircraft under gust. First, the design of a longitudinal control system for automatic landing is presented for a linear aircraft model. Then, the fuzzy controller parameters derived for the linear model are modified to obtain a robust control system for a six degree of freedom nonlinear aircraft model. It is shown that the simple tuning fuzzy controller, by altering scaling factors, is well suited for control of difficult aircraft maneuvers like landing in severe weather conditions which require continuous change in engine thrust and control surfaces.

AB - Fuzzy logic based control system is developed for glideslope capture of an aircraft under gust. First, the design of a longitudinal control system for automatic landing is presented for a linear aircraft model. Then, the fuzzy controller parameters derived for the linear model are modified to obtain a robust control system for a six degree of freedom nonlinear aircraft model. It is shown that the simple tuning fuzzy controller, by altering scaling factors, is well suited for control of difficult aircraft maneuvers like landing in severe weather conditions which require continuous change in engine thrust and control surfaces.

UR - http://www.scopus.com/inward/record.url?scp=84983111507&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:84983111507

T2 - 37th Aerospace Sciences Meeting and Exhibit, 1999

Y2 - 11 January 1999 through 14 January 1999

ER -

Glideslope capture in wind gust via fuzzy logic controller

Abstract

Conference

Other files and links

Fingerprint

Cite this