AIRCRAFT LANDING GEAR DYNAMICS - SIMULATION AND CONTROL

Citation
W. Kruger et al., AIRCRAFT LANDING GEAR DYNAMICS - SIMULATION AND CONTROL, Vehicle System Dynamics, 28(2-3), 1997, pp. 119-158
Citations number
83
Categorie Soggetti
Engineering, Mechanical
Journal title
ISSN journal
00423114
Volume
28
Issue
2-3
Year of publication
1997
Pages
119 - 158
Database
ISI
SICI code
0042-3114(1997)28:2-3<119:ALGD-S>2.0.ZU;2-#
Abstract
The landing gear is an inevitable system for the aircraft. It absorbs the energy of the landing impact and carries the aircraft weight at al l ground operations, including take off, taxiing, and towing, Numerica l simulation has become an invaluable tool for the assessment of landi ng gear dynamics as well as of aircraft/landing gear interaction. This paper gives an overview of the landing gear requirements and illustra tes landing gear operational conditions, i.e., the shimmy problem, the dynamics at touch down and at ground roll. Furthermore, three softwar e packages used in the simulation of aircraft ground dynamics are pres ented. A look at flight simulators and landing gear test facilities fo llows. Finally, the possible application of controlled landing gears i s discussed.