DocumentCode
2783443
Title
Modeling and simulation for arrested landing of carrier-based aircraft
Author
Lv, Kaidong ; Zhu, Qidan ; Li, Xinfei
Author_Institution
Coll. of Autom., Harbin Eng. Univ., Harbin, China
fYear
2011
fDate
7-10 Aug. 2011
Firstpage
1928
Lastpage
1933
Abstract
Mathematical model of a hydraulic arresting gear system on aircraft carrier is constructed. The constant runout control valve device which is the most important part of arresting gear system is studied. In the following, a simulation model based on the mathematical model is set up, and simulation experiments are carried out. It is turned out that: the hydraulic arresting gear system can recover a landing aircraft in the constant distance of 67 m on the flight deck, provided its weight is in the range of 50, 000 pound and its engaging velocity is within the limit of 110 knots.
Keywords
aircraft; gears; hydraulic systems; valves; aircraft carrier; arrested landing; carrier-based aircraft; constant runout control valve device; hydraulic arresting gear system; landing aircraft; mathematical model; Acceleration; Aircraft; Equations; Gears; Mathematical model; Random access memory; Valves; aircraft weight selector; arrested landing; carrier-based aircraft; constant runout control valve; engaging velocity;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2011 International Conference on
Conference_Location
Beijing
ISSN
2152-7431
Print_ISBN
978-1-4244-8113-2
Type
conf
DOI
10.1109/ICMA.2011.5986275
Filename
5986275
Link To Document