DocumentCode
1806947
Title
Robust aircraft pitch-axis control under weight and center of gravity uncertainty
Author
Khammash, M. ; Zou, L. ; Almquist, J.A. ; Van Der Linden, C.
Author_Institution
Dept. of Electr. & Comput. Eng., Iowa State Univ., Ames, IA, USA
Volume
2
fYear
1999
fDate
1999
Firstpage
1970
Abstract
Robust control of aircraft longitudinal (pitch) attitude is presented. The discussion focuses on the longitudinal attitude control problem when aircraft weight and center of gravity are varying over a specified range. Due to the variation of weight and center of gravity in aircraft models, multiplicative uncertainty models are derived for robust synthesis. Pitch attitude robust controllers are designed to provide consistent performance under varying weight and varying center of gravity locations
Keywords
H∞ control; aircraft control; attitude control; control system synthesis; robust control; center of gravity uncertainty; consistent performance; longitudinal attitude control; robust aircraft pitch-axis control; robust synthesis; weight uncertainty; Aerospace control; Aircraft propulsion; Attitude control; Control system synthesis; Elevators; Gravity; Robust control; Robustness; Uncertainty; Weight control;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1999. Proceedings of the 38th IEEE Conference on
Conference_Location
Phoenix, AZ
ISSN
0191-2216
Print_ISBN
0-7803-5250-5
Type
conf
DOI
10.1109/CDC.1999.830925
Filename
830925
Link To Document