DocumentCode
3041497
Title
Application of magneto-rheological (MR) damper in landing gear shimmy
Author
Chen Da-wei ; Gu Hong-bin ; Wu Hao
Author_Institution
Nanjing Univ. of Aeronaut. & Astronaut., Nanjing, China
fYear
2010
fDate
8-10 June 2010
Firstpage
1212
Lastpage
1216
Abstract
In order to study the semi-active control of landing gear shimmy, expressions of MR damper equivalent damping coefficient with voltage and amplitude was set up firstly. And then, the mathematical model for semi-active control of landing gear shimmy was constructed and maximum energy dissipation approach based on MR was proposed to suppress shimmy. Finally, the critical shimmy velocity varying with the vertical force during taxiing was investigated in different caster lengths. The simulation results show that the performance of MR to suppress shimmy is greatly superior to hydraulic shimmy damper during taxiing, and MR not only suppresses shimmy completely but also exhibits good robustness about some system parameters.
Keywords
aerospace control; hydraulic control equipment; magnetorheology; robust control; shock absorbers; vibration control; caster length; critical shimmy velocity; damping coefficient; hydraulic shimmy damper; landing gear shimmy; magnetorheological damper; mathematical model; maximum energy dissipation; semiactive control; taxiing; vertical force; Aircraft; Damping; Force; Gears; Mathematical model; Shock absorbers; Wheels; magneto-rheological (MR) damper; maximum energy dissipation; robustness; semi-active; shimmy;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5633047
Filename
5633047
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