DocumentCode
2044197
Title
Nonlinear control of an aircraft in the presence of microburst windshear
Author
Yamagishi, Satoshi ; Hasegawa, Naoki ; Sakamoto, Noboru ; Sato, Masayuki
Author_Institution
Dept. of Aerosp. Eng., Nagoya Univ., Nagoya, Japan
fYear
2011
fDate
13-18 Sept. 2011
Firstpage
1029
Lastpage
1034
Abstract
This paper presents a climb-rate guidance scheme for aircraft flight through a microburst windshear on final approach. The control law will be developed using a new method derived from stable manifold theory to solve a Hamilton-Jacobi equation approximately. Simulation results demonstrate that the aircraft can safely transit severe microburst windshear by obtained nonlinear optimal control law.
Keywords
aerospace materials; aircraft control; aircraft landing guidance; nonlinear control systems; optimal control; stability; Hamilton-Jacobi equation; aircraft flight climb-rate guidance scheme; aircraft nonlinear control; microburst windshear; nonlinear optimal control law; stable manifold theory; Aerospace control; Airplanes; Atmospheric modeling; Equations; Mathematical model; Optimal control; Flight Control; Nonlinear Control; Wind Shear;
fLanguage
English
Publisher
ieee
Conference_Titel
SICE Annual Conference (SICE), 2011 Proceedings of
Conference_Location
Tokyo
ISSN
pending
Print_ISBN
978-1-4577-0714-8
Type
conf
Filename
6060660
Link To Document