DocumentCode
3783815
Title
Antiskid control for aircraft via extremum-seeking
Author
I. Tunay
Author_Institution
Dept. of Syst. Sci. & Math., Washington Univ., St. Louis, MO, USA
Volume
2
fYear
2001
fDate
6/23/1905 12:00:00 AM
Firstpage
665
Abstract
A novel method of antiskid control for transport aircraft is proposed. After robustly stabilizing the hydraulics using an inner-loop controller based on feedback linearization and H/sub /spl infin// theory, a sinusoidal signal of small amplitude is injected into the brake pressure to estimate, in real-time, tyre-runway friction properties. This information is used by the algorithm to keep the friction coefficient slightly less than the maximum allowed by the runway conditions. This results in much smoother braking compared to controllers currently in operation, which try to reach the maximum. Consequently, passenger comfort will be improved and component wear will be reduced, while achieving comparable or better stopping performance. In some cases, several hundred feet of improvement in stopping distance is possible, as demonstrated via realistic simulations based on a detailed model of the MD-90 aircraft.
Keywords
"Aerospace control","Tires","Wheels","Friction","Aircraft manufacture","Gears","Torque","Control systems","Robust control","Pressure control"
Publisher
ieee
Conference_Titel
American Control Conference, 2001. Proceedings of the 2001
ISSN
0743-1619
Print_ISBN
0-7803-6495-3
Type
conf
DOI
10.1109/ACC.2001.945790
Filename
945790
Link To Document