DocumentCode
3079605
Title
Aircraft control under conditions of windshear
Author
Leitmann, George ; Pandey, Sandeep
Author_Institution
Dept. of Mech. Eng., California Univ., Berkeley, CA, USA
fYear
1990
fDate
5-7 Dec 1990
Firstpage
747
Abstract
The design of the control of an aircraft encountering windshear after takeoff is treated as a problem of stabilizing the climb rate about a desired value of the climb rate. The resulting controller is a feedback one utilizing only climb rate information. Its robustness namely windshear structure and intensity is illustrated via simulations employing four different windshear models. The simulations were carried out for the Boeing 727 aircraft
Keywords
aircraft control; control system synthesis; feedback; stability; Boeing 727; aircraft control; climb rate; design; feedback; robustness; stability; windshear; Aerospace control; Aircraft propulsion; Control systems; FAA; Feedback; Mechanical engineering; Robustness; Uncertain systems; Uncertainty; Wind speed;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1990., Proceedings of the 29th IEEE Conference on
Conference_Location
Honolulu, HI
Type
conf
DOI
10.1109/CDC.1990.203687
Filename
203687
Link To Document